AIAA IEEE Digital Avionics Systems Conference: 12th DASC
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| Corporate Author: | |
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| Format: | Conference Proceeding Book |
| Language: | English |
| Published: |
Piscataway, NJ
Inst. of Electrical and Electronics Engineers
1993
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| Subjects: | |
| Online Access: | Inhaltsverzeichnis |
| Physical Description: | 480 S. Ill., graph. Darst. |
| ISBN: | 0780313437 0780313445 |
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| 111 | 2 | |a Digital Avionics Systems Conference |n 12 |d 1993 |c Seattle, Wash. |j Verfasser |0 (DE-588)5111820-8 |4 aut | |
| 245 | 1 | 0 | |a AIAA IEEE Digital Avionics Systems Conference |b 12th DASC |
| 246 | 1 | 3 | |a 12th DASC |
| 246 | 1 | 3 | |a Twelfth DASC |
| 246 | 1 | 3 | |a Digital Avionics Systems Conference |
| 264 | 1 | |a Piscataway, NJ |b Inst. of Electrical and Electronics Engineers |c 1993 | |
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| adam_text | Table of Contents
Systems Engineering: Industry
Direction and Experiences
Co-Chairmen:
Synthetic Vision
Co-Chairmen:
Paul Gartz
has been responsible for systems
engineering processes, methods
and tools architecture at the
Boeing Commercial Airplane
Group. He is chairman and Presi¬
dent of the Structured Develop¬
ment Forum, Inc., a charter mem¬
ber of the National Council on Sys¬
tems Engineering. Paul earned an
M.S. in electrical engineering from
Stanford and performed postgrad¬
uate work in psychology and
business.
Brian Mar
has been teaching systems eng¬
ineering for over
25
years at the
University of Washington. Prior to
joining the University, he was
employed at the Boeing Company
for ten years, He is currently the
President of the National Council
of Systems Engineers and has
been a consultant to Aerospace
environmental and government
agencies on systems engineering.
Photograph Unavailable
This session will review new directions of major corporations, industry
standards, project experiences and lessons learned in the systems
engineering discipline. Specific methods and tools will be discussed
regarding benefits to the overall systems engineering process.
Experience with software systems will be addressed only as an element
of the overall systems engineering process.
DoD Standards for Avionics Systems
Architectures
B. Jewett
Keys to Meeting the Operational Enhancement
Needs of the Air Traffic Management
Systems
A. ElSawy
IEEE
Ρ
1220—
Standard for Systems
Engineering
—
A Commercial Standard for
Improving Competitiveness
R. Schmidt
Systems Engineering Positions—Honeywell
Air Transport Systems Division for the Future
G. Tsikalas and L. Sherry
A Renewed Focus on Systems Engineering
—
Efforts Within Boeing Commercial Airplane
Group
M. Redmond
12
17
John Todd Brian
Hartman
Since joining Douglas Aircraft is a Systems Engineer at Hughes
Company in
1986,
Mr. Todd has Flight Dynamics. He obtained a
been working in the Advanced B.S. in Physics from the University
Design Integration section of the of California at Riverside.
Flight Controls Technology group.
He is presently program manager
of fly-by-light/power-by-wire sys¬
tems. Mr. Todd holds B.S. degrees
in
ЕЕ
and geophysics from Wright
State University, as well as M.A.
and B.A. degrees in anthropology
from Miami University, and Univer¬
sity of Arizona, respectively.
This session will focus on advanced guidance and control systems
for improved aircraft operations and situational awareness with special
emphasis on landing, takeoff, and taxi capabilities during adverse
weather and low visibility. Papers will address commercial and military
needs, near and longer term R&D of sensors and navigation aids and
their fusion, displays, the human/machine interface, and system
integration .
Enhanced/Synthetic Vision for Transport
21
Aircraft
J.A. Todd, J.A. Hay, W.L Wallace and
L.G. Summers
Head-Up Guidance Systems: Foundation of
f
Situation Awareness Systems
B.K.
Hartman
Certification of the FEC Civil Stroke and Raster
t
Read-Up Display
T. Bushnell
Wide-Eye™ Head-Mounted Display for
27
Rotorcraft Applications
L. Zintmaster
Airline Operations and Economics in Low
f
Visibility
W. Syblon
Honeywell/Westinghouse Enhanced
τ
Situational Awareness Flight Test
Experience
F.N. Gomer
Enhanced Vision Systems: Advantages and
ţ
Current Developments
L
Baron
Forward Looking Sensors for Enhanced and
Synthetic Vision Systems
J.L.
Armitage
Enhanced Situational Awareness: A Cockpit
Operations Perspective
D.R.
Beins
Sensors and Signal Processing
Co-Chairmen:
Pilot-Automation Interface:
A Potential Killing Zone
Co-Chairmen:
Edward
Truj i
Ilo
is the Program Manager of
Advanced Avionics Systems at
Hughes Aircraft Co., and has
27
years experience in avionics
systems design and management.
He holds a B.S. in
ЕЕ
form the
University of California at Berkeley
and has performed graduate
studies at the University of South¬
ern California. He was recently
selected Chairman of the AIAA
Digital Avionics Technical Com¬
mittee and is a member of IEEE
and ACM.
Leonard Carlson
has over
25
years of engineering
and management experience in
aerospace and defense electron¬
ics. He is currently Manager,
Advanced Projects Engineering at
United Technologies Corp.-Nor-
den Systems, and is currently re¬
sponsible for development of ad¬
vanced airport systems. Mr.
Carlson holds a B.S. and M.S. in
ЕЕ
from New York University.
Avionics represents a significant portion of the costs associated with
modern aircraft. New concepts in sensors and signal processing are
aimed at reducing these costs but at the same time pushing technology
into new frontiers for the next century.
Integrated Sensor Fusion
ţ
R.F.
Popoli
and
S.C.
Oxford
Sensor Management
32
R.
A. Adrian
Ultra Reliable Digital Avionics
38
G.P. Rubertus
The Adaptive Multiprocessing System (AMPS)
43
W. Vojir and J. Wedgewood
Architecture Evaluation through the Use of
49
Simulation Environment Benchmarking
C.A. Sweeney
Wavelets
—
A New Tool for Signal Processing
54
Analysts
M. Colestock
Jack Maher
is presently a Boeing
767
Line
Check Airman Captain with Delta
Airlines, has
17,000
hours in the
cockpit, and is doing human fac¬
tors research at Harvard University
and the University of Texas/NASA
Aerospace Crew Research Cen¬
ter. He has a B.S. in economics
from Holy Cross College.
Bob North
is a section chief of the Crew Sys¬
tems and Maintenance Diagnos¬
tics Section at Honeywell Systems
and Research Center in Minneap¬
olis, MN. Dr. North is currently
working on several FAA programs
in flightdeck automation design
ethods including the areas of
flight mode enunciation, flight
management system interface,
crew workload estimation, and ac¬
cident investigation. Dr. North re¬
ceived his Ph.D. in engineering
psychology from the University of
Illinois.
Considerable evidence exists linking flight crew misunderstanding of
automated systems to accidents, incidents, or abnormal situations.
Although automation of many fucntions over the history of aviation has
enabled modern aircraft to achieve highly reliable and safe means of
transport, the pilot (crew) has beocme less involved in direct control of
these functions. The crew is more susc eptible to false assumptions and
inadvertent actions leading to a host of potential problems. This session
will feature research results, anecdotal evidence, and design methods
for the philosophy of human-centered automation and implications for
design of future avionics systems.
Pilot Error in Automated Systems Shown by
60
Altitude Deviation Reports
R.
Ritter
Cockpit Automation—The Pilot s Perspective
t
B.A. Mayhew
Functional Categories for Human-Centered
66
Flight Deck Design
T.S. Abbott and W.H. Rogers
Function Allocation Issues and Tradeoffs:
t
A Design Methodology for Human Centered
Automation
V. Riley
From Data to Information: Data Reduction
75
for Operator Workload Management
W. Terry, J.K. Terry and L.G. Cable
Aeronautical Communications:
The Critical Path
Co-Chairmen:
Commercial Avionics I
Co-Chairmen:
Pete Camana
is the Advanced Systems Manager
for Communications, Navigation
and Identification
(CNI)
at TRW/
MEAD, and is responsible for
technical direction and program
acquisition in the
CNI
area. He
holds a B.S. in
ЕЕ
from Lehigh Uni¬
versity, an M.S. in
ЕЕ
and a Ph.D.
from Ohio State University.
Jim Dieudonne
is department head of
АТС
Com¬
munication Systems and joined
MITRE in
1979.
He earned a B.S.
in physics from the University of
Southwestern Louisiana, an M.S.
in
ЕЕ
from George Washington
University, and completed Ph.D.
requirements in
ЕЕ
from the Uni¬
versity of Virginia.
With the civilian move to an ATM system which utilizes improved flight
crew and flight management system capabilities, and increased
cooperative military actions, communications to and from the aircraft
has become the critical path for success of flight missions. In addition
to these increases, there is a steady move to digital data and satellite
links for worldwide seamless coverage. This session addresses current
and future technology improvements in this arena.
Scott
Rausch
is an Engineering Department
Manager for Honeywell Air
Transport Systems Division. He
has
14
years of CRT and LCD
cockpit display experience in both
general aviation and air transport
application. Scott has a BSEE
degree from South Dakota School
of Mines and Technology.
Steve
Runo
is a systems Engineer for SCITOR
(Sunnyvale, CA) supporting
Boeing
777
Airplane Systems In¬
tegration. Before joining SCITOR,
Mr.
Runo
was Honeywell s Tech¬
nical Manager for flight manage¬
ment development. Mr.
Runo
graduated from Harvey Mudd Col¬
lege (Claremont, CA), and studied
in Seattle University s Masters pro¬
grams in software engineering and
business administration.
This session, and its companion session Commercial Avionics II, focus
on application of technology to the commercial avionics marketplace.
Authors present information from programs that are under development
or are in service. Lessons learned and other results are often reported.
FAA s Design Approach to a Global Data Link
81
System
E. Shochet
A Database Approach to Diagnostics in an
ł
Integrated
CNI
System
D. Secor and J. Byloff
Integrated
CNI
Avionics for the F-22
ł
CA.
Wolfe and M.E. Campbell
Improved VHF Air/Ground Communications
86
System: Technical Tradeoffs
B. Eckstein, D.J. Chadwick,
L
delCid, J.C. Moody
and B.E. White
ATM and
FIS
Data Link Services
92
C.
Bauhof
Innovative Approaches for Implementing the
98
Aeronautical Telecommunications Network
S.
Gallegos, W.B.
Link and D. Thomson
ADS-Mode Systems Overview
104
R.E. Boisvert and V.A. Orlando
Meeting Airlines Needs Using Avionics
f
Retrofit
J.
Sneed
Boeing
777
AIMS: An Update
f
J. Carter and R. Robertson
Deutsch
Airbus Flight Test of Rosemount
110
Smart Probe for Distributed Air Data Systems
F. Hagen
and H.
Seidel
Enhancing Visual Approaches with the TC AS
t
Traffic Display
J.
Cie
plak
Airborne Positioning and Planning System:
t
An Approach to Simplifying Future Flight
Operations
G.W. Fiathers,
II
ARINC
629
Integration forthe Boeing
777
t
S.
Runo
Modular
Avionics
Co-Chairmen
:
Artificial Intelligence and
Expert Systems
Chairman:
Glen Logan
Photograph and
Biography Unavailable
Gene Harvey
is a Senior Principal Engineer with
Arine Reserach
Corporation,
supporting the Modular Avionics
Architecture
(MASA)
Program
Office for the last five years. He
received a Bachelor of Engineering
degree from Youngstown Univer¬
sity in Ohio, and a master s degree
in Management Science from the
University of Dayton. He is also a
graduate of the Program Manage¬
ment Course at the Defense Sys¬
tems Management College.
Modular avionics architectures promise to provide an infrastructure
for cost-effective, mission-capable and -adaptable avionics systems for
the future. This session highlights several recent developments in
modular avionics technology for new as well as inventory aircraft.
Virtual Test Stations (VTS)
118
S.A.
Walters
The Reliable Optical Card-Edge Connector
124
(ROC)
S.
Benning,
R.J.
Pimpinella
and J.D. Seals
Programmable Channelized Digital Radio for
t
Modular Avionics Retrofit Market
R.W. Minarik
An Ada Run-Time Environment Supporting
129
the Development of Verifiable Realtime
Software for Embedded Modular Avionics
Systems
P. Little and J.D. Preston
A Practical Object-Oriented Approach for
135
Distributed Real Time Simulation
S.A.
Walters
Ed Huff
is a Senior Scientist in the Information
Sciences Division at NASA s Ames Re¬
search Center. During his career with
NASA, Dr. Huff served in various Branch-
and Division-level management posi¬
tions. In
1989,
he received the Comman¬
der s Medal from the US Army, AVSCOM
for his efforts in the Helicopter/VTOL
Human Factors program. He completed
graduate work in experimental and
mathematical psychology at the Univer¬
sity of Buffalo and Texas Christian Univer¬
sity. His present goal is to further research
in real-time human-computer dialog, telepresence and telecontrol, and
adaptive model-based reasoning.
During the past decade, several Artificial Intelligence methods, most
notably expert systems and similar types of heuristic reasoning, have
been proposed for a variety of advanced in-flight and ground-based
aeronautical applications. In addition to expert systems, this session will
consider a broad sampling of other intelligent system methodologies,
such as neural networks, cognitive modeling, and pattenr recognition to
improve human-computer interaction, message prioritization, decision
aiding, adaptive control, and fault diagnosis.
FINDER: A System Providing Complex
141
Decision Support for Commercial Transport
Replanning
Operations
V. Bitterman, G.
Deker, P. Sassus, J.C. Mielnikand
J-M.
Jud
A New Adjudicator for Fault Tolerant Software
147
Applications Correctly Resulting in Multiple
Solutions
L. Pullum
The Fourth-Dimensional Cockpit
153
J.W. Voorhees, A.L.
Zaklad, M.Z.
Weiland,
W.W. Zachary
and
CA.
Fry
Development of an Intelligent System to Aid
160
in Avionics Display Design
S.P. Rogers and L.D. Myers
Artificial Intelligence and Expert Systems for
167
Avionics
L. Harrison, P.J.
Saraceni,
Jr., and P.J. Saunders
Application of Neural Networks to Flight
t
Control Systems Synthesis
R.J.
Montoya
and J.W. Watterson
HIRF
Testing
Co-Chairmen:
Commercial
Avionics II
Co-Chairmen:
Ken Grachan
is currently the lead systems en¬
gineer on the KFC
500
Automatic
Flight Control System for the Bell
230
Helicopter at Allied signal Aer¬
ospace. Mr. Grachan received a
B.S. in engineering from the Uni¬
versity of Illinois and an M.S. in
electrical engineering from the Il¬
linois Institute of Technology. He is
also an active member of SAE and
RTCA committees.
Gerry Fuller
is a senior consultant on the staff
of CKC Laboratories, Inc., where
he conducts research and devel¬
ops seminars and technical papers
on HIRF. He is currently develop¬
ing and teaching advanced HIRF
design and testing seminars, and
conducts research into coupling of
R F
energy into
airframes
and av¬
ionics systems on civilian aircraft.
Mr. Fuller holds both a BSEE and
MSEE from the University of Mary¬
land, and completed his course
work as a Ph.D. candidate in
ЕЕ
and physics.
This session will focus on the modern control methods applicable to
the incorporation of HIRF protection into aircraft designs in a cost-
effective manner. Papers will address the issues of susceptibility, test
costs, and the effects of HIRF requirements with respect to new aircraft
certifications and to certification involving modifications of existing
aircraft.
Microwave Induced Upset of a Digital Control
173
Computer
B.T. Clough
Microwave Induced Upset of Digital Flight
179
Control Systems
B. Clough, B. Cope and S. Donley
Effects of High Power Microwaves to Flight
t
Control Sensors
B. Cope
Application of Numerical Analysis to the
185
Electromagnetic Effects Validation of Aircraft
R.A. Perala,
Т.Н.
Rudolph, P.M. McKenna and
С
Jones
A Study of Occurrence Rates of EMI to Aircraft
191
with a Focus on HIRF
M.L. Shooman
System Level HIRF Testing
197
P.C.
Scott
Steve
Runo
is a Systems Engineer for SCITOR
(Sunnyvale, CA) supporting
Boeing
777
Airplane Systems Inte¬
gration. Before Joining SCITOR,
Mr.
Runo
was Honeywell s Tech¬
nical Manager for flight manage¬
ment development. Mr.
Runo
graduated from Harvey Mudd Col¬
lege (Claremont, CA), and studied
in Seattle University s Masters
programs in software engineering
and business administration.
Scott
Rausch
is an Engineering Department
Manager for Honeywell Air
Transport Systems Division. He
has
14
years of CRT and LCD
cockpit display experience in both
general aviation and air transport
applications. Scott has a BSEE
degree from South Dakota School
of Mines and Technology.
This session, and its companion session Commercial Avionics I, focus
on application of technology to the commercial avionics marketplace.
Authors present information from programs that are under development
or are in service. Lessons Learned and other results are often reported.
Digital Air-Ground Communications for VHF
203
Air Traffic Control
J.W. Howland
Preliminary Requirements for Satellite Based
209
Automatic Dependent Surveillance (ADS)
G. Bartkiewica and R. Berkowitz
The Gospel According to DO-178B
t
J.
Treacy
Integration of Cursor Control Device
t
Technology on Boeing
777
Cockpit Displays
I. Fenwich and D. Prescott
Application of GPS
t
J.
Jackson
Fault Tolerant
Avionics
Co-Chairmen
:
Rotorcraft
Avionics
Co-Chairmen:
Larry Ott Mike
Beach
is the
Manager
of the Signal
Proc-
Photograph and
essor
Computer Systems Tech- Biography Unavailable
nology Division at the Naval Air
Warfare Center, Warminster, PA.
Mr. Ott
has been with the Navy for
over
30
years, and is responsible
for the development and applica¬
tions of those technologies that get
information from the sensors on
the aircraft to the operator. He has
a M.A. in physics and an M.B.A. in
management.
This session will describe how fault tolerance can be implemented
not only at the subsystem level but also for the entire avionics system.
Papers will discuss fault tolerant techniques along with the status of
ongoing laboratory experiments.
Status of the Advanced Avionics Subsystem
215
Technology
(AAST)
Fault Tolerant
Demonstration
T. Monoghan
Reducing the Probability of Common-Mode
221
Failure in the Fault Tolerant Parallel Processor
J.H.
Lala
and R.E. Harper
Fault Tolerant Virtual Machine Architecture for
231
Advanced Avionics Applications
J. Ozols and D.A. Pederson
Computer Upset, Matrix Norms, and
237
Asymptotic Stability
A. White
Application of Distributed, Fault Tolerant
243
Ada to Multiprocessor, Real-Time, Integrated
Avionics Systems
K.L. Nelson and L.M. Meredith
Accommodation of Non-Universal Input Data
248
Errors in Cross-Strapped Redundant
Computer Systems through Forward Error
Correction Coding
J.N. Yelverton
A Simulated Life-Validation Experiment for
254
Fault-Tolerant Systems
A.L. White
Richard Coppenbarger
has been with the Aircraft Guid¬
ance and Navigation branch at
NASA Ames Research Center for
five years. His primary areas of re¬
search have been automatic ob¬
stacle avoidance guidance, pilot-
system interface, and head-up dis¬
plays. He received a B.S. in aero¬
space engineering from the Uni¬
versity of Arizona and an M.S. in
aerospace engineering from
Stanford.
Bob Jacobsen
received his undergraduate and
graduate degrees from the Univer¬
sity of California, Berkeley. Mr.
Jacobsen joined NASA-Ames Re¬
search Center in July
1967
as an
Aerospace Scientist and has been
responsible for research in the
areas of flight dynamics, aircraft
controls and aircraft guidance. He
is now Project Manager for the
RASCAL research helicopter.
As the next century approaches, civil and military rotorcraft missions
will become increasingly complex, demanding even greater pilot skill
and attention. It will be the roll of advanced avionic technology to counter
the trend towards higher cockpit workload and provide for enhanced
levels of performance and safety. Situational awareness will continue
to be a primary concern to rotorcraft pilots who frequently fly at low
altitudes under adverse environmental conditions. Papers in this session
will focus upon advanced sensors, displays, and associated avionic
systems to provide pilots with increased knowledge of their position and
surrounding to aid in navigation, route planning, obstacle avoidance,
and fire control.
The AN/ASN-1
57:
A Single LRU
Doppler
260
Navigation System for Helicopters
H. Buell and D. Doremus
Simulation Development of a Forward
267
Sensor-Enhanced Low-Altitude Guidance
System
R.
Zelenka,
H.N.
Swenson, M.G. Dearing and
G.H. Hardy
Simulation of Obstacle Avoidance System
276
(OASYS) Sensor and Display Alternatives
J.M. Hughes
Synthetic Vision for Improving Flight Control
286
in Night, Poor Visibility and Adverse Weather
Conditions
H.
Möller
and G. Sachs
Computer Architectures for a Real-Time
292
Passive Ranging Algorithm
B. Sridhar and R.E. Suorsa
Rotorcraft Aerial Robot
—
Challenges and
298
Solutions
M. Gordon, S.
Kondor,
E.
Corban and D.
Schrage
Cockpit Technology
Co-Chairmen:
Optical
Technology
Co-Chairmen:
Ellis
Hitt
is Chief Engineer on Battelle s
Design Engineering Program
Contract with the Air Force Mater¬
ial Command, as well as Avionics
Systems Engineering Business
Development Manager for the De¬
fense Systems Engineering and
Technology. Mr.
Hitt
earned a B.S.
in electrical engineering from the
University of Kansas, and received
the M.S. in electrical engineering
from the Air Force Institute of
Technology.
Hugh
Moreland
Colonel, USAF (Ret.), joined
General Dynamics in
1987
as
Manager of F-17 Pilot-Vehicle
Integration (PVI), and in
1992,
his
duties increased to include dir¬
ecting the effort of the PVI Section.
He holds a B.S. in chemistry from
Louisiana Polytechnic Institute, is
a graduate of the ROTC program,
and completed pilot training at
Webb Air Force Base, Texas.
Technology in Transition
—
Controls and displays are continuing the
transition from analog to digital technology in both commercial and
military aircraft. Commercial aircraft lead the way in the application of
new technology to cockpits with the number of new commercial aircraft
starts far exceeding military aircraft starts. New cockpit technology is
beginning to be retrofit into military aircraft which poses challenges and
opportunities for the military. The move from mechanical display of
aircraft state to automated cockpits to situational awareness, provides
the need for new research and standards. The present graphical
presentations with dynamic foreground and background making use of
color leads to the future visual presentation of automatic picture based
on information priority of crew selected multiple windows.
Boeing
777
Flight Deck
t
R.
Houck
C-1
41
Glass Cockpit
t
В.
Gadbois
Digital Flat Panel Cockpit Displays and
306
Specification
D. Hopper
New Cockpit Technology: How do We Really
312
Know It Benefits the Pilot?
T.J.
Solz,
J. Reising, K.K. Liggett and D.C. Hartsock
Fighter Cockpit of the Future
318
E.C. Adam
Cockpit Information Management in the
t
F-1
6
Aircraft
J.S. Eckel and J.E.
Hartman
Flight Assessment of
3
Flat Panel Display
475
Technologies for CRT Replacement
T. Stauffer, E.
Hitt
and F.
Rea
Chuck Meissner
is the head of the System Valida¬
tion Methods Branch (SVMB) at
NASA Langley Research Center.
He has been employed at NASA
Langley since
1958
working pri¬
marily in aircraft instrumentation
and flight systems, and has
headed SVMB for the past
7
years.
He received a BS in
ЕЕ
from Vir¬
ginia Polytechnic Institute, and an
MS in
ЕЕ
from Stanford University.
Felix Pitts
is a senior research engineer and
specialist in electronic systems
engineering and lightning charac¬
terization and effects at NASA
Langley. He is the author or co¬
author of
17
publications and
1
patent, and received a NASA
Exceptional Engineering Medal.
He earned a BS in
ЕЕ
from the Uni¬
versity of Alabama, and did gradu¬
ate work at the Univ. of Virginia.
Fiberoptics is the fundamental enabling technology for Fly-By-Light
(FBL) systems on aircraft. The aim of FBL is the replacement of electronic
data transmission and electronic sensors with optical components and
subsystems. The intrinsic immunity of optical technology embodied in
FBL can mitigate EMI concerns of HIRF effects on digitally controlled
systems while providing lifetime immunity to signal EMI. This session
will cover fundamental aspects such as connectors, sensors, photonics,
and signaling, as well as the role of the tgechnologies in enabling features
of FBL systems to be realized. Significant issues with applying these
technologies will be discussed.
Photonic Integrated Circuits for Wide
324
Bandwidth Avionic Systems
W. Rideout, W. Powazinik and J. LaCourse
Optical Connectors and Variable Losses in
329
Coupling Multimode Fibers
R.
Pimpinella
and
E.E. Bergmann
Airborne Photonics, A Technology Whose
336
Time Has Come
A. Glista
Fiber Optic Position Sensing for Engine and
343
Flight Controls
S.
Emo
and J. Gustus
Photonics Technology
f
or Avionic Systems
349
G.L. Abbas, C.S. Hong, G.E. Miller, C.R. Porter,
S. Ray, M.C. Reddy, D.K. Smith and L. Figueroa
Fly-By-Light Installation and Maintenance
357
on Transport Aircraft
J. Todd, J.C. Pilatos,
JA.
White and N.L. Hug
System
Integration
and Testing
Co-Chairmen:
Current Space Systems
Chairman:
James Branstetter
is an aerospace engineer at NASA
Langley Research Center, and
manages cooperative research
projects of a multidisciplinary na¬
ture including simulation and flight
testing of approach procedures for
use with MLS, airborne sensing of
wake-vortices, wind tunnel testing
of radar propagation in heavy rain,
and prototyping the pilot s auto¬
mated weather support system.
Wade Duym
is an Aerospace Engineering Duty
Officer in the US Navy. He is
currently assigned to the Naval
Postgraduate School, Monterey,
CA as Aerospace Engineering
Curricular
Officer. Commander
Duym is a Naval Aviator who holds
a MS in Systems Technology and
is completing a MS in Engineering
Science. He is a Senior Member of
AIAA and has been active with the
DATC since May
1992.
This session provides experiences in, applications of existing
techniques to, and develompent of new capabilities for, the integration
and testing of distributed system software and software components.
Unique Applications of Custom MIL-STD-
1553 363
ASIC
K. Brittain, D. Dalnodar and R.
Sottile
Selection and Demonstration of a Common
368
Data Bus Monitor and Analysis System
J.
Gromada
and T. Pham
Specification of Sampled Data System Timing
375
Parameters for Hard Real-Time Avionics
Systems
T. Smith
Improving Software Development Through the
382
Proper Implementation of a Standard Software
Process: Case Study and Lessons Learned
E. Safford
Current Trends and Practices in Ramp Testing
388
of Digital Avionics Systems
A.
Helfrick
Advanced Graphics Processor
394
K.R. Runyon
Nikolas Bletsos
is the Manager of the Booster Guidance
Section of the Guidance Analysis Depart¬
ment of the Aerospace Corporation. He
has been with The Aerospace Corpora¬
tion since
1979,
after three years with
Rockwell International on the Space
Shuttle program. He received a B.S., M.S.
and Ph.D. in Aerospace Engineering from
the University of Michigan, specializing in
hypervelocity entry dynamics and control.
Photograph Unavailable
This session focuses on the current state of technology and technology
achievements and development efforts capable of impacting space sci¬
entific and exploration missions, including ground support operations
and technologies, in the near- to medium-term future.
The
Ariane 5
Avionics Architecture
t
Y. Durand
Wind Velocity Estimation Through Onboard
t
Measurements
R.M. DeLeonardis
Practical Applications of Modern Controls for
400
Booster Autopilot Design
MA deVirgilio
and D.K. Kamimoto
A Summary of Spacecraft Avionics
413
Functions
J.F. Smith
Airport Surface Operations
Chairman:
Software Engineering
Co-Chairmen:
Leonard Carlson
has over
25
years of engineering and
management experience as well, in
aerospace and defense electronics. He
is currently Manager, Advanced Projects
Engineering at United Technologies Cor-
poration-Norden Systems. He is currently
responsible for development of advanced
airport systems at
Norden.
Mr. Carlson
holds BS and MS degrees in electrical
engineering from New York University
and has taken advanced courses at the
University of Connecticut and the Hartford
Graduate Center.
Safe and efficient traffic movement on the airport surface, particularly
under poor weather conditions, is a major concern throughout the aviation
world. This session addresses systems under development to enhance
airport surface safety and traffic flow including the use of aircraft/vehicle
and ground based equipment.
Sensor Technology and Air Traffic Safety
t
C.
Hilterbrick
Surface Movement and Route Tracking—
t
Automation for the Tower CAB
D. Grisckowsky
Differential GPS Based Precision Approaches
t
and Surface Operational Trials
J.L Kendrick
Computerized Airport Tracking System
t
(CATS)
D.M.
Brown
In Integrated Radio-Location Packet Data
419
Network with Potential for Application to
Surface Traffic Management at Commercial
Airports
LH.M. Jandrell
Airport Surface Collision Warning System
425
Implementation
J. lanniello and R.
Kruczek
A Multi-Sensor Approach to Airport Surface
430
Traffic Tracking
D. Stauffer, H. French, J.
Lenz
and G. Rouse
LesDupaix
is currently a consultant on Ada
and Software Engineering issues
at the U.S. Air Force Software
Technology Support Center at Hill
Air Force Base, Utah. He received
a BS in
ЕЕ
from Brigham Young
University.
Linda
Alger
is Division Manager of the Soft¬
ware Engineering Division of The
Charles Stark Draper Laboratory,
She is responsible for system soft¬
ware, and the system integration
and testing of the Seawolf
(SSN-1
2)
Ship Control Processing
Unit.
This session features tools, techniques, and methodologies for the
efficient development of distributed avionics software. The emphasis in
this session is on the automation of the development process (including
requirements traceability), aids for the transition of design to code, and
techniques and methodologies for the management of progress in the
design and development phase of a project.
Using Software Document Evaluations to
Enhance Software Supportability
F.C. Budlong and J.J.
Stanko
Towards a Framework for the Post-
Deployment Software Support of Air Force
Embedded Systems
S. Friend
Systems/Software Engineering Environment
A.P. Hyatt
Process-Centered Engineering Environment
for Avionics Software Development
G. Brannum
Object-Oriented Programming in Ada
J.
Irwin
LCA Avionics Design Methods, Tools, and
Prototyping
B.C. Banerji
433
t
t
t
t
Fly-By-Light
/
Power-By-Wire
Co-Chairmen:
Vehicle Management Systems
Co-Chairmen:
Felix Pitts
¡s a
senior research engineer and
specialist in electronic systems
engineering and lightning charac¬
terization and effects at NASA
Langley. He is the author or co¬
author of
17
publications and
1
pat¬
ent, and received a NASA Excep¬
tional Engineering Achievement
Medal. He earned a BS in
ЕЕ
from
the University of Alabama, and did
graduate work at University of
Virginia.
Chuck Meissner
is the head of the System Valida¬
tion Methods Branch (SVMB) at
NASA Langley Research Center.
He has been employed at NASA
Langley since
1958
working pri¬
marily in aircraft instrumentation
and flight systems, and has
headed SVMB for the past
7
years.
He received a BS in
ЕЕ
from Vir¬
ginia Polytechnic Institute, and an
MS in
ЕЕ
from Stanford University.
The objective of the Fly-By-Light/Power-By-Wire (FBUPBW) session
is to present snapshots and overview information of the state and
application of technologies which will enable advancements in transport
aircraft employing FBL/PBW. This session will build on the optical
technology base, and cover the fundamental aspects of PBW such as
motor control, actuators, and power systems technology, include a
discussion of residual EMI relative to computers, and culminate with
requirements for modern FBL/PBW systems.
Power-By-Wire Motor Control and Technology
t
R.
Lorenz
Technical Requirements for Fly-By-Light/
t
Power-By-Wire Systems
I. Reese
Power-By-Wire Aircraft Secondary Power
439
Systems
L.
Feiner
Electrical Power Technology for the More
445
Electric Aircraft
J. Weimer
A Methodology for Assessing High Intensity
451
RF Effects in Aircraft
R.
Zacharias, CA.
Avalle,
K.S.
Kunz, N.E.
Molati,
ST. Pennock, A.J.
Poggio
and R.M.
Sharpe
Integrating Fly-By-Light Power-By-Wire Flight
457
Control Systems on Transport Aircraft
J. Todd, J.A. Hay and T. Dinh
Anthony
DeThomas
is a senior engineer in the Wright
Laboratory Flight Control Division.
He holds a Ph.D. and MS in
Electrical Engineering and a
BSEE. His professional experi¬
ence encompasses research in
sensor technologies, flight control
hardware and software, systems
integration, VMS, and advanced
control applications.
John Weyrach
is the manager of the Systems and
Control Sciences department
within Honeywell s Systems and
Research Center in Minneapolis,
Minnesota, and has worked in the
aerospace industry for
20
years.
He worked for McDonnell Douglas
for nine years, and for the last
11
years has been with Honeywell
where he has performed research
on advanced VMS concepts and
ultra-reliable navigation systems.
This session will concentrate on the technologies related to the
integration of vehicle control and management functions. Papers will
address research on architectural, functional, and simulation
technologies and how they relate to Vehicle Management System
development.
YF-22/F-22 Vehicle Management System
t
D.
Harbour
Warni
ng System Concepts to Prevent
463
Controlled Flight Into Terrain (CFIT)
C.S. Young
The
F-HľAAutof
light System
t
K.G. Gousman and R. Rooney
Digital Terrain System Flight Test
t
Demonstration on the F 16B Aircraft
J.E. Lay, T. Suanders, M. Couch and J. Balakirsky
Development of a Full-Envelope, Automatic,
t
All-Terrain Ground Collision Avoidance
System
DP, Browning and M.R. Griswold
An Approach to Aircraft Subsystems Design
469
and Integration
D.A.
Busch
and J.F.
Áldana
t
Manuscript unavailable for publication.
Author Index
Abbas, G.L
...............349
Abbott, T.S
................66
Adam, E.C
................318
Adrian, R.A
................32
Áldana,
J.F...............
469
Avalle,
CA
................451
Bartkiewica,
G.............
209
Bauhof,
С
.................92
Benning,
S
................124
Bergmann, E.E............329
Berkowitz,
R..............
209
Bitterman,
V
...............141
Boisvert,
R.E..............104
Brittain,
К
.................363
Budlong, F.C
..............433
Buell,
H..................
260
Busch, D.A...............469
Cable,
LG.................75
Chadwick, DJ..............86
Clough,
В.............
173, 179
Colestock,
M...............
54
Соре, В
..................179
Corban, E
................298
Dalnodar,
D...............
363
Dearing,
M.G..............
267
Deker, G
.................141
del Cid, L
..................86
de Virgilio, M.A
............400
Dinh,
T
...................457
Donley,
S
.................179
Doremus,
D
...............260
Eckstein,
В
................86
El Sawy,
A
..................1
Emo,
S
...................343
Feiner,
L
.................439
Figueroa,
L
...............349
French,
H
.................430
Fry,
CA
..................153
Gallegos,
S
................98
Glista,
A
..................336
Gordon, M
................298
Gromada,
J...............
368
Gustus,
J.................
343
Hagen, F
.................110
Hardy,
G.H...............
267
Harper,
R.E...............221
Harrison,
L
................167
Hartsock,
D.C
.............312
Hay, J.A
...............21, 457
Helfrick,
A
................388
Hong,
CS................
349
Hopper, D
................306
Howland,
J.W.............
203
Hug, N.L
.................357
Hughes,
J.M..............
276
lanniello,
J................
425
Jandrell, L.H.M............
419
Jones, C
.................185
Jud,
J-M
..................141
Kamimoto,
D.
К............
400
Kondor,
S
................298
Kruczek, R
................425
Kunz, K.S................451
LaCourse,
J
...............324
Lala,
J.H
.................221
Lenz, J...................430
Liggett,
К.К
...............312
Link,
W.B
..................98
Little,
P
..................129
McKenna,
P.M
.............185
Meredith,
L.M
.............243
Mielnik,
J-C
...............141
Miller,
G.E................349
Molau,
N.E................451
Möller,
H
.................286
Monoghan,
T
..............215
Moody,
J.C
................86
Myers,
LD
................160
Nelson, K.L
...............243
Orlando, V.A
..............104
Ozols,
J
..................231
Pederson, D.A
.............231
Pennock, S.T
..............451
Perala, R.A
...............185
Pham,
T
..................368
Pilatos, J.C
...............357
Pimpinella,
R..........
124, 329
Poggio, A.J
...............451
Porter, C.R
...............349
Powazinik, W
..............324
Preston,
J.D
...............129
Pullum, L
.................147
Ray. S
...................349
Reddy, M.C
...............349
Redmond, M
...............17
Reising,
J
.................312
Rideout,
W
................324
Ritter, R...................60
Rogers, S.P...............160
Rogers, W.H...............66
Rouse,
G.................
430
Rubertus, G.P..............38
Rudolph, T.H..............185
Runyon, K.R..............394
Sachs,
G
.................286
Safford,
E
................382
Saraceni, P.J.,
Jr
...........167
Sassus,
P
................141
Saunders,
P J
.............167
Schmidt,
R
..................6
Schrage,
D
...............298
Scott,
P.C
................197
Seals,
J.D
................124
Seidel,
H
.................110
Sharpe,
R.M
..............451
Sherry, L
..................12
Shochet, E
.................81
Shooman, M.L
.............191
Smith, D.K
................349
Smith, J.F
................413
Smith, T
..................375
Solz,
TJ
.................312
Sottile,
M.R
...............363
Todd,
J
.......... 21
,
357, 457
White, A
..............237, 254
Sridhar,
В
................292
Tsikalas, G
................12
White, B.E
.................86
Stanko,
J.J
................433
White, J.A
................357
Stauffer,
D
................430
Vojir,
W
...................43
Summers, L.G
..............21
Voorhees, J.W
.............153
Yelverton, J.N
.............248
Suorsa, R.E
...............292
Young, C.S
...............463
Sweeney, C.A
..............49
Wallace, W.L
...............21
Swenson, H.N
.............267
Walters, S.A
..........118, 135
Zacharias,
R..............
451
Wedgewood,
J
..............43
Zachary,
W.W
.............153
Terry,
J.K
..................75 Weiland, M.Z..............153
Zaklad, A.L
...............153
Terry,
W
...................75
Weimer,
J
................445
Zelenka, R
................267
Thomson,
D
................98
Zintmaster, L
...............27
|
| any_adam_object | 1 |
| author_corporate | Digital Avionics Systems Conference Seattle, Wash |
| author_corporate_role | aut |
| author_facet | Digital Avionics Systems Conference Seattle, Wash |
| author_sort | Digital Avionics Systems Conference Seattle, Wash |
| building | Verbundindex |
| bvnumber | BV011339614 |
| callnumber-first | T - Technology |
| callnumber-label | TL693 |
| callnumber-raw | TL693 |
| callnumber-search | TL693 |
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| callnumber-subject | TL - Motor Vehicles and Aeronautics |
| classification_tum | VER 625f |
| ctrlnum | (OCoLC)29434849 (DE-599)BVBBV011339614 |
| dewey-full | 629.135 |
| dewey-hundreds | 600 - Technology (Applied sciences) |
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| dewey-raw | 629.135 |
| dewey-search | 629.135 |
| dewey-sort | 3629.135 |
| dewey-tens | 620 - Engineering and allied operations |
| discipline | Verkehrstechnik Verkehr / Transport |
| format | Conference Proceeding Book |
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| genre_facet | Konferenzschrift 1993 |
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| illustrated | Illustrated |
| indexdate | 2024-07-09T18:08:04Z |
| institution | BVB |
| institution_GND | (DE-588)5111820-8 |
| isbn | 0780313437 0780313445 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-007618956 |
| oclc_num | 29434849 |
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| owner | DE-91 DE-BY-TUM |
| owner_facet | DE-91 DE-BY-TUM |
| physical | 480 S. Ill., graph. Darst. |
| publishDate | 1993 |
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| publisher | Inst. of Electrical and Electronics Engineers |
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| spelling | Digital Avionics Systems Conference 12 1993 Seattle, Wash. Verfasser (DE-588)5111820-8 aut AIAA IEEE Digital Avionics Systems Conference 12th DASC 12th DASC Twelfth DASC Digital Avionics Systems Conference Piscataway, NJ Inst. of Electrical and Electronics Engineers 1993 480 S. Ill., graph. Darst. txt rdacontent n rdamedia nc rdacarrier Digital avionics Congresses Avionik (DE-588)4196491-3 gnd rswk-swf (DE-588)1071861417 Konferenzschrift 1993 gnd-content Avionik (DE-588)4196491-3 s DE-604 Digitalisierung TU Muenchen application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=007618956&sequence=000002&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | AIAA IEEE Digital Avionics Systems Conference 12th DASC Digital avionics Congresses Avionik (DE-588)4196491-3 gnd |
| subject_GND | (DE-588)4196491-3 (DE-588)1071861417 |
| title | AIAA IEEE Digital Avionics Systems Conference 12th DASC |
| title_alt | 12th DASC Twelfth DASC Digital Avionics Systems Conference |
| title_auth | AIAA IEEE Digital Avionics Systems Conference 12th DASC |
| title_exact_search | AIAA IEEE Digital Avionics Systems Conference 12th DASC |
| title_full | AIAA IEEE Digital Avionics Systems Conference 12th DASC |
| title_fullStr | AIAA IEEE Digital Avionics Systems Conference 12th DASC |
| title_full_unstemmed | AIAA IEEE Digital Avionics Systems Conference 12th DASC |
| title_short | AIAA IEEE Digital Avionics Systems Conference |
| title_sort | aiaa ieee digital avionics systems conference 12th dasc |
| title_sub | 12th DASC |
| topic | Digital avionics Congresses Avionik (DE-588)4196491-3 gnd |
| topic_facet | Digital avionics Congresses Avionik Konferenzschrift 1993 |
| url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=007618956&sequence=000002&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
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