H aerospace control design: a VSTOL flight application
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Buch |
| Sprache: | German |
| Veröffentlicht: |
Berlin ; Heidelberg ; New York ; Barcelona ; Budapest ; Hong Kon
Springer
1995
|
| Schriftenreihe: | Advances in industrial control
|
| Schlagworte: | |
| Online-Zugang: | Inhaltsverzeichnis |
| Beschreibung: | Literaturverz. S. 211 - 214 |
| Beschreibung: | XVI, 216 S. graph. Darst. |
| ISBN: | 3540199608 |
Internformat
MARC
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| 100 | 1 | |a Hyde, Richard Alden |e Verfasser |4 aut | |
| 245 | 1 | 0 | |a H aerospace control design |b a VSTOL flight application |c R. A. Hyde |
| 264 | 1 | |a Berlin ; Heidelberg ; New York ; Barcelona ; Budapest ; Hong Kon |b Springer |c 1995 | |
| 300 | |a XVI, 216 S. |b graph. Darst. | ||
| 336 | |b txt |2 rdacontent | ||
| 337 | |b n |2 rdamedia | ||
| 338 | |b nc |2 rdacarrier | ||
| 490 | 0 | |a Advances in industrial control | |
| 500 | |a Literaturverz. S. 211 - 214 | ||
| 650 | 4 | |a Flight control | |
| 650 | 4 | |a H [infinity symbol] control | |
| 650 | 4 | |a Short take-off and landing aircraft |x Automatic control | |
| 650 | 4 | |a Vertically rising aircraft |x Automatic control | |
| 650 | 0 | 7 | |a V/STOL-Flugzeug |0 (DE-588)4124405-9 |2 gnd |9 rswk-swf |
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| 689 | 0 | |5 DE-604 | |
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Datensatz im Suchindex
| _version_ | 1807865606506020864 |
|---|---|
| adam_text |
CONTENTS
PART
I.
DESIGN
AND
IMPLEMENTATION
OF
CONTROLLERS
1.
INTRODUCTION
.
3
2.
THE
MOTIVATION
FOR
ROBUST
CONTROL
.
7
2.1
INTRODUCTION
.
7
2.2
MULTIVARIABLE
CONTROL
.
8
2.2.1
MOTIVATION
.
8
2.2.2
LIMITATIONS
OF
GAIN
AND
PHASE
MARGINS
.
9
2.2.3
EXTENSION
OF
CLASSICAL
DESIGN
TO
MULTIVARIABLE
PLANTS
.
9
2.3
DESIGN
IN
H
X
.
10
2.3.1
USING
SINGULAR
VALUES
AS
A
ROBUSTNESS
MEASURE
.
10
2.3.2
THE
H
X
STANDARD
PLANT
.
12
2.3.3
THE
S
&
KS
DESIGN
PROCEDURE
.
13
2.3.4
THE
LOOP-SHAPING/COPRIME
FACTOR
UNCERTAINTY
APPROACH
15
2.4
THE
STRUCTURED
SINGULAER
VALUE
.
16
2.5
SUMMARY
.
17
3.
A
MULTIVARIABLE
DESIGN
GASE
STUDY
.
19
3.1
AN
INTRODUCTION
TO
VSTOL
AIRCRAFT
.
19
3.2
THE
GENERIC
VSTOL
AIRCRAFT
MODEL
(GVAM)
.
20
3.3
FLIGHT
CONTROL
MODES
.
21
3.4
HANDLING
QUALITIES
.
24
3.4.1
INTRODUCTION
.
24
3.4.2
THE
AGARD
AND
MIL-SPECIFICATIONS
.
24
3.4.3
THE
GIBSON
CRITERIA
.
27
3.5
GVAM
NON-LINEARITIES
.
28
3.5.1
INTRODUCTION
.
28
3.5.2
KEY
PARAMETERS
.
28
3.5.3
ENGINE
GOVERNOR
.
29
3.5.4
THRUST
RESOLUTION
.
30
3.5.5
BANK
ANGLE
COMPENSATION
.
31
3.5.6
OTHER
NON-LINEARITIES
.
31
3.6
UNCERTAINTY
MODELLING
.
31
3.6.1
UNSTRUCTURED
UNCERTAINTY
.
31
XIV
TABLE
OF
CONTENTS
3.6.2
STATE-SPACE
UNCERTAINTY
MODELLING
.
32
3.7
A
SPECIFICATION
FOR
LINEAR
FEEDBACK
DESIGN
.
33
3.8
SUMMARY
.
35
4.
ROBUST
DESIGN
USING
LOOP-SHAPING
.
37
4.1
INTRODUCTION
.
37
4.2
A
LOOP-SHAPING
PROCEDURE
.
38
4.2.1
THE
PROCEDURE
.
38
4.2.2
ILL-CONDITIONED
PLANTS
.
40
4.2.3
CONTROLLER
POSITIONING
IN
THE
LOOP
.
41
4.2.4
SCALING
.
42
4.3
JUSTIFICATION
OF
THE
PROCEDURE
.
43
4.4
FREUDENBERG
'
S
GUIDELINES
.
44
4.5
EXTRA
MEASUREMENTS
.
46
4.5.1
AN
EXAMPLE
SYSTEM
.
46
4.5.2
COMPLEMENTARY
FILTER
APPROACH
.
47
4.5.3
A
LOOP-SHAPING
APPROACH
.
48
4.5.4
HOW
THE
APPROACHES
COMPARE
.
48
4.6
GVAM
HOVER
DESIGN
EXAMPLE
.
50
4.6.1
APPLICATION
OF
THE
DESIGN
PROCEDURE
.
50
4.6.2
REFLECTION
OF
HQ
REQUIREMENTS
IN
THE
PROCEDURE
.
51
4.6.3
ROBUST
PERFORMANCE
ANALYSIS
.
56
4.7
FRACTIONAL
DISTILLATION
COLUMN
EXAMPLE
.
56
4.8
SUMMARY
.
60
5.
CONTROLLER
SWITCHING
.
63
5.1
INTRODUCTION
.
63
5.2
BUMPLESS
TRANSFER
USING
THE
HANUS
APPROACH
.
64
5.2.1
THE
HANUS
APPROACH
.
64
5.2.2
IMPLEMENTATION
OF
LOOP-SHAPING
CONTROLLERS
.
65
5.2.3
LIMITATIONS
OF
THE
APPROACH
.
66
5.2.4
SELECTING
THE
'
D
'
-MATRIX
.
67
5.2.5
RELATIONSHIP
TO
THE
HIGH
GAIN
APPROACH
.
68
5.3
GVAM
SWITCHED
CONTROLLER
EXAMPLE
.
69
5.3.1
THE
LINEAR
DESIGNS
.
69
5.3.2
LINEAR
ANALYSIS
.
69
5.3.3
IMPLEMENTATION
IN
TSIM
.
69
5.4
STABILITY
ANALYSIS
.
72
5.4.1
A
STABILITY
ANALYSIS
TECHNIQUE
FOR
SWITCHING
.
72
5.4.2
APPLICATION
TO
THE
GVAM
EXAMPLE
.
74
5.5
SUMMARY
.
76
TABLE
OF
CONTENTS
XV
6.
CONTROLLER
SCHEDULING
.
77
6.1
INTRODUCTION
.
77
6.2
SCHEDULING
USING
AN
OBSERVER
STRUCTURE
.
78
6.2.1
WRITING
LOOP-SHAPING
CONTROLLERS
AS
OBSERVERS
.
78
6.2.2
SCHEDULING
ON
SEVERAL
PARAMETERS
.
81
6.2.3
LIMITATIONS
OF
THE
APPROACH
.
81
6.3
GVAM
DESIGN
EXAMPLES
.
81
6.3.1
SCHEDULING
ON
FORWARD
SPEED
.
81
6.3.2
SCHEDULING
ON
SPEED
AND
INCIDENCE
.
83
6.4
A
LINEAR
ANALYSIS
TECHNIQUE
FOR
SCHEDULED
CONTROLLERS
.
88
6.4.1
THE
ANALYSIS
PROCEDURE
.
88
6.4.2
APPLICATION
TO
THE
FORWARD
SPEED
SCHEDULE
.
91
6.5
SUMMARY
.
93
7.
MULTIVARIABLE
ANTI-WINDUP
.
95
7.1
SATURATING
ACTUATORS
ON
MULTIVARIABLE
SYSTEMS
.
95
7.2
A
FRAMEWORK
FOR
ANTI-WINDUP
ANALYSIS
.
96
7.3
APPLICATION
OF
HANUS
'
APPROACH
.
98
7.4
VARIABLE
LOOP-GAIN
APPROACH
.
99
7.5
OBSERVER
APPROACH
.
99
7.6
PRIORITISED
APPROACH
.
101
7.7
SUMMARY
.
102
8.
CONTROLLER
COMPLEXITY
.
103
8.1
INTRODUCTION
.
103
8.2
IMPLEMENTATION
USING
A
DISCRETE
MODAL
FORM
.
104
8.3
COMPLEXITY
OF
THE
SWITCHING
AND
SCHEDULING
APPROACHES
.
105
8.4
A
DESIGN
STUDY
USING
FIXED
STRUCTURE
CONTROLLERS
.
107
8.4.1
A
MULTI
OBJECTIVE
PROGRAMMING
SYSTEM
(MOPS)
.
107
8.4.2
DESIGNS
USING
MOPS
.
107
8.4.3
A
COMPARISON
OF
H
X
AND
MOPS
DESIGNS
.
109
8.4.4
CONCLUSIONS
FROM
THE
MOPS
DESIGN
STUDY
.
118
8.5
SUMMARY
.
119
PART
II.
A
FLIGHT
CONTROL
LAW
FOR
THE
DRA
XW175
RESEARCH
HARRIER
9.
BACKGROUND
.
123
10.
LINEAR
DESIGN
AND
ANALYSIS
.
125
10.1
FEEDBACK
VARIABLES
.
125
10.2
ROVER
DESIGN
.
129
10.3
SPECIFICATIONS
FOR
THE
LINEAR
DESIGNS
.
136
10.4
JUSTIFICATION
FOR
USING
MULTIVARIABLE
DESIGN
.
137
XVI
TABLE
OF
CONTENTS
11.
DISCRETISATION
.
145
11.1
SAMPLING
AT
50
HZ
.
145
11.2
SAMPLING
AT
25
HZ
.
147
12.
FLIGHT
CONTROL
MODES
AND
COMMAND
PRECOMPENSATION
.
153
12.1
FLIGHT
MODES
FOR
005
.
153
12.2
THE
LEFT-HAND
INCEPTOR
.
157
12.3
THE
RIGHT-HAND
INCEPTOR
.
159
12.4
TRIM-SWITCH
AND
PITCH
HOLD
.
160
13.
LIMITERS
AND
NON-LINEAR
ASPECTS
.
163
13.1
ENGINE
COMPENSATOR
.
163
13.2
DESATURATION
SCHEME
.
164
13.3
LIMITERS
.
165
13.3.1
DESCENT
RATE
LIMITER
.
165
13.3.2
LOW
THROTTLE
LIMIT
.
165
13.3.3
INVERTED
FLYING
PROTECTION
.
165
13.4
THRUST/ATTITUDE
TRIM
ALGORITHM
.
166
13.5
FORWARD
NOZZLE
IN
WINGBORNE
FLIGHT
.
167
13.6
HAND-OVER
LOGIC
.
167
13.7
FEEDFORWARD
OF
BANK
ANGLE
.
168
13.8
HEIGHT-HOLD
.
168
13.9
FEEDFORWARD
FROM
NOZZLES
TO
TAILPLANE
.
168
13.10PERFORMANCE
MEASUREMENT
POINTS
.
169
13.11LANDING
LOGIC
.
169
13.12IMPLEMENTATION
IN
FORTRAN
AND
CORAL
.
169
14.
UNPILOTED
TIME
SIMULATION
.
173
14.1
CONTROL
LAW
INITIALISATION
.
173
14.2
MANOEUVRE
TESTING
.
174
14.3
TRANSITION
TESTING
.
174
14.4
EFFECT
OF
SENSOR
NOISE
.
175
14.5
ROBUSTNESS
EVALUATION
.
175
15.
PILOTED
SIMULATION
AND
FLIGHT
TESTING
.
191
15.1
SIMULATOR
RESULTS
.
191
15.2
FLIGHT
TEST
RESULTS
.
194
16.
CONCLUSIONS
.
199
A.
LIST
OF
VARIABLES
.
203
B.
BLOCK
DIAGRAM
.
209
REFERENCES
.
211
INDEX
.
215 |
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| id | DE-604.BV010475527 |
| illustrated | Illustrated |
| indexdate | 2024-08-20T00:49:54Z |
| institution | BVB |
| isbn | 3540199608 |
| language | German |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-006979940 |
| oclc_num | 32431925 |
| open_access_boolean | |
| owner | DE-91G DE-BY-TUM DE-706 DE-83 |
| owner_facet | DE-91G DE-BY-TUM DE-706 DE-83 |
| physical | XVI, 216 S. graph. Darst. |
| publishDate | 1995 |
| publishDateSearch | 1995 |
| publishDateSort | 1995 |
| publisher | Springer |
| record_format | marc |
| series2 | Advances in industrial control |
| spelling | Hyde, Richard Alden Verfasser aut H aerospace control design a VSTOL flight application R. A. Hyde Berlin ; Heidelberg ; New York ; Barcelona ; Budapest ; Hong Kon Springer 1995 XVI, 216 S. graph. Darst. txt rdacontent n rdamedia nc rdacarrier Advances in industrial control Literaturverz. S. 211 - 214 Flight control H [infinity symbol] control Short take-off and landing aircraft Automatic control Vertically rising aircraft Automatic control V/STOL-Flugzeug (DE-588)4124405-9 gnd rswk-swf Flugregelung (DE-588)4328094-8 gnd rswk-swf V/STOL-Flugzeug (DE-588)4124405-9 s Flugregelung (DE-588)4328094-8 s DE-604 DNB Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=006979940&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Hyde, Richard Alden H aerospace control design a VSTOL flight application Flight control H [infinity symbol] control Short take-off and landing aircraft Automatic control Vertically rising aircraft Automatic control V/STOL-Flugzeug (DE-588)4124405-9 gnd Flugregelung (DE-588)4328094-8 gnd |
| subject_GND | (DE-588)4124405-9 (DE-588)4328094-8 |
| title | H aerospace control design a VSTOL flight application |
| title_auth | H aerospace control design a VSTOL flight application |
| title_exact_search | H aerospace control design a VSTOL flight application |
| title_full | H aerospace control design a VSTOL flight application R. A. Hyde |
| title_fullStr | H aerospace control design a VSTOL flight application R. A. Hyde |
| title_full_unstemmed | H aerospace control design a VSTOL flight application R. A. Hyde |
| title_short | H aerospace control design |
| title_sort | h aerospace control design a vstol flight application |
| title_sub | a VSTOL flight application |
| topic | Flight control H [infinity symbol] control Short take-off and landing aircraft Automatic control Vertically rising aircraft Automatic control V/STOL-Flugzeug (DE-588)4124405-9 gnd Flugregelung (DE-588)4328094-8 gnd |
| topic_facet | Flight control H [infinity symbol] control Short take-off and landing aircraft Automatic control Vertically rising aircraft Automatic control V/STOL-Flugzeug Flugregelung |
| url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=006979940&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
| work_keys_str_mv | AT hyderichardalden haerospacecontroldesignavstolflightapplication |