Flight dynamics principles /:
The study of flight dynamics requires a thorough understanding of the theory of the stability and control of aircraft, an appreciation of flight control systems and a comprehensive grounding in the theory of automatic control. Flight Dynamics provides all three in an accessible and student focussed...
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Elektronisch E-Book |
| Sprache: | English |
| Veröffentlicht: |
Amsterdam ; Boston :
Elsevier/Butterworth-Heinemann,
2007.
|
| Ausgabe: | 2nd ed. |
| Schriftenreihe: | Elsevier aerospace engineering series.
|
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Zusammenfassung: | The study of flight dynamics requires a thorough understanding of the theory of the stability and control of aircraft, an appreciation of flight control systems and a comprehensive grounding in the theory of automatic control. Flight Dynamics provides all three in an accessible and student focussed text. Written for those coming to the subject for the first time the book is suitable as a complete first course text. It provides a secure foundation from which to move on to more advanced topics such a non-linear flight dynamics, simulation and advanced flight control, and is ideal for tho. |
| Beschreibung: | 1 online resource (xxi, 468 pages) : illustrations |
| Bibliographie: | Includes bibliographical references and index. |
| ISBN: | 9780080550367 0080550363 |
Internformat
MARC
| LEADER | 00000cam a2200000 a 4500 | ||
|---|---|---|---|
| 001 | ZDB-4-EBA-ocn179872855 | ||
| 003 | OCoLC | ||
| 005 | 20241004212047.0 | ||
| 006 | m o d | ||
| 007 | cr cnu---unuuu | ||
| 008 | 071030s2007 ne a ob 001 0 eng d | ||
| 040 | |a N$T |b eng |e pn |c N$T |d YDXCP |d OCLCQ |d OCLCF |d OCLCO |d OCLCQ |d AGLDB |d Z5A |d JBG |d LIP |d OCLCQ |d VTS |d CEF |d STF |d M8D |d UHL |d UKAHL |d OCLCQ |d OCLCO |d OCLCQ |d OCLCO |d OCLCL |d OCLCQ | ||
| 019 | |a 173264081 |a 1113311457 | ||
| 020 | |a 9780080550367 |q (electronic bk.) | ||
| 020 | |a 0080550363 |q (electronic bk.) | ||
| 035 | |a (OCoLC)179872855 |z (OCoLC)173264081 |z (OCoLC)1113311457 | ||
| 050 | 4 | |a TL570 |b .C66 2007eb | |
| 072 | 7 | |a TRA |x 002000 |2 bisacsh | |
| 082 | 7 | |a 629.132/3 |2 22 | |
| 049 | |a MAIN | ||
| 100 | 1 | |a Cook, M. V. | |
| 245 | 1 | 0 | |a Flight dynamics principles / |c M.V. Cook. |
| 250 | |a 2nd ed. | ||
| 260 | |a Amsterdam ; |a Boston : |b Elsevier/Butterworth-Heinemann, |c 2007. | ||
| 300 | |a 1 online resource (xxi, 468 pages) : |b illustrations | ||
| 336 | |a text |b txt |2 rdacontent | ||
| 337 | |a computer |b c |2 rdamedia | ||
| 338 | |a online resource |b cr |2 rdacarrier | ||
| 490 | 1 | |a Elsevier aerospace engineering series | |
| 504 | |a Includes bibliographical references and index. | ||
| 588 | 0 | |a Print version record. | |
| 505 | 0 | 0 | |t Flight Dynamics Principles -- |t Copyright page -- |t Preface to the first edition -- |t Preface to the second edition -- |t Nomenclature -- |g 1. |t Introduction -- |g 1.1. |t Overview -- |g 1.2. |t Flying and handling qualities -- |g 1.3. |t General considerations -- |g 1.4. |t Aircraft equations of motion -- |g 1.5. |t Aerodynamics -- |g 1.6. |t Computers -- |g 1.7. |t Summary -- |g 2. |t Systems of axes and notation -- |g 2.1. |t Earth axes -- |g 2.2. |t Aircraft body fixed axes -- |g 2.3. |t Euler angles and aircraft attitude -- |g 2.4. |t Axes transformations -- |g 2.5. |t Aircraft reference geometry -- |g 2.6. |t Controls notation -- |g 2.7. |t Aerodynamic reference centres |
| 505 | 0 | 0 | |g 5.1. |t Methods of solution -- |g 5.2. |t Cramer's rule -- |g 5.3. |t Aircraft response transfer functions -- |g 5.4. |t Response to controls -- |g 5.5. |t Acceleration response transfer functions -- |g 5.6. |t The state space method -- |g 5.7. |t State space model augmentation -- |t Problems -- |g 6. |t Longitudinal dynamics -- |g 6.1. |t Response to controls -- |g 6.2. |t The dynamic stability modes -- |g 6.3. |t Reduced order models -- |g 6.4. |t Frequency response -- |g 6.5. |t Flying and handling qualities -- |g 6.6. |t Mode excitation -- |t Problems -- |g 7. |t Lateral-directional dynamics -- |g 7.1. |t Response to controls -- |g 7.2. |t The dynamic stability modes -- |g 7.3. |t Reduced order models |
| 505 | 0 | 0 | |g 7.4. |t Frequency response -- |g 7.5. |t Flying and handling qualities -- |g 7.6. |t Mode excitation -- |t Problems -- |g 8. |t Manoeuvrability -- |g 8.1. |t Introduction -- |g 8.2. |t The steady pull-up manoeuvre -- |g 8.3. |t The pitching moment equation -- |g 8.4. |t Longitudinal manoeuvre stability -- |g 8.5. |t Aircraft dynamics and manoeuvrability -- |g 9. |t Stability -- |g 9.1. |t Introduction -- |g 9.2. |t The characteristic equation -- |g 9.3. |t The Routh-Hurwitz stability criterion -- |g 9.4. |t The stability quartic -- |g 9.5. |t Graphical interpretation of stability -- |t Problems -- |g 10. |t Flying and handling qualities -- |g 10.1. |t Introduction |
| 505 | 0 | 0 | |g 10.2. |t Short term dynamic models -- |g 10.3. |t Flying qualities requirements -- |g 10.4. |t Aircraft role -- |g 10.5. |t Pilot opinion rating -- |g 10.6. |t Longitudinal flying qualities requirements -- |g 10.7. |t Control anticipation parameter -- |g 10.8. |t Lateral-directional flying qualities requirements -- |g 10.9. |t Flying qualities requirements on the s-plane -- |t Problems -- |g 11. |t Stability augmentation -- |g 11.1. |t Introduction -- |g 11.2. |t Augmentation system design -- |g 11.3. |t Closed loop system analysis -- |g 11.4. |t The root locus plot -- |g 11.5. |t Longitudinal stability augmentation -- |g 11.6. |t Lateral-directional stability augmentation -- |g 11.7. |t The pole placement method. |
| 520 | |a The study of flight dynamics requires a thorough understanding of the theory of the stability and control of aircraft, an appreciation of flight control systems and a comprehensive grounding in the theory of automatic control. Flight Dynamics provides all three in an accessible and student focussed text. Written for those coming to the subject for the first time the book is suitable as a complete first course text. It provides a secure foundation from which to move on to more advanced topics such a non-linear flight dynamics, simulation and advanced flight control, and is ideal for tho. | ||
| 650 | 0 | |a Aerodynamics. |0 http://id.loc.gov/authorities/subjects/sh85001295 | |
| 650 | 0 | |a Flight control. |0 http://id.loc.gov/authorities/subjects/sh85049111 | |
| 650 | 0 | |a Stability of airplanes. |0 http://id.loc.gov/authorities/subjects/sh85127186 | |
| 650 | 6 | |a Aérodynamique. | |
| 650 | 6 | |a Systèmes de commande (Vol) | |
| 650 | 6 | |a Avions |x Stabilité. | |
| 650 | 7 | |a aerodynamics. |2 aat | |
| 650 | 7 | |a TRANSPORTATION |x Aviation |x General. |2 bisacsh | |
| 650 | 7 | |a Aerodynamics |2 fast | |
| 650 | 7 | |a Flight control |2 fast | |
| 650 | 7 | |a Stability of airplanes |2 fast | |
| 776 | 0 | 8 | |i Print version: |a Cook, M.V. |t Flight dynamics principles. |b 2nd ed. |d Amsterdam ; Boston : Elsevier/Butterworth-Heinemann, 2007 |z 0750669276 |z 9780750669276 |w (OCoLC)171268192 |
| 830 | 0 | |a Elsevier aerospace engineering series. | |
| 856 | 4 | 0 | |l FWS01 |p ZDB-4-EBA |q FWS_PDA_EBA |u https://search.ebscohost.com/login.aspx?direct=true&scope=site&db=nlebk&AN=203095 |3 Volltext |
| 938 | |a Askews and Holts Library Services |b ASKH |n AH25540755 | ||
| 938 | |a EBSCOhost |b EBSC |n 203095 | ||
| 938 | |a YBP Library Services |b YANK |n 2703626 | ||
| 994 | |a 92 |b GEBAY | ||
| 912 | |a ZDB-4-EBA | ||
| 049 | |a DE-863 | ||
Datensatz im Suchindex
| DE-BY-FWS_katkey | ZDB-4-EBA-ocn179872855 |
|---|---|
| _version_ | 1816881655260905472 |
| adam_text | |
| any_adam_object | |
| author | Cook, M. V. |
| author_facet | Cook, M. V. |
| author_role | |
| author_sort | Cook, M. V. |
| author_variant | m v c mv mvc |
| building | Verbundindex |
| bvnumber | localFWS |
| callnumber-first | T - Technology |
| callnumber-label | TL570 |
| callnumber-raw | TL570 .C66 2007eb |
| callnumber-search | TL570 .C66 2007eb |
| callnumber-sort | TL 3570 C66 42007EB |
| callnumber-subject | TL - Motor Vehicles and Aeronautics |
| collection | ZDB-4-EBA |
| contents | Flight Dynamics Principles -- Copyright page -- Preface to the first edition -- Preface to the second edition -- Nomenclature -- Introduction -- Overview -- Flying and handling qualities -- General considerations -- Aircraft equations of motion -- Aerodynamics -- Computers -- Summary -- Systems of axes and notation -- Earth axes -- Aircraft body fixed axes -- Euler angles and aircraft attitude -- Axes transformations -- Aircraft reference geometry -- Controls notation -- Aerodynamic reference centres Methods of solution -- Cramer's rule -- Aircraft response transfer functions -- Response to controls -- Acceleration response transfer functions -- The state space method -- State space model augmentation -- Problems -- Longitudinal dynamics -- The dynamic stability modes -- Reduced order models -- Frequency response -- Mode excitation -- Lateral-directional dynamics -- Reduced order models Manoeuvrability -- The steady pull-up manoeuvre -- The pitching moment equation -- Longitudinal manoeuvre stability -- Aircraft dynamics and manoeuvrability -- Stability -- The characteristic equation -- The Routh-Hurwitz stability criterion -- The stability quartic -- Graphical interpretation of stability -- Introduction Short term dynamic models -- Flying qualities requirements -- Aircraft role -- Pilot opinion rating -- Longitudinal flying qualities requirements -- Control anticipation parameter -- Lateral-directional flying qualities requirements -- Flying qualities requirements on the s-plane -- Stability augmentation -- Augmentation system design -- Closed loop system analysis -- The root locus plot -- Longitudinal stability augmentation -- Lateral-directional stability augmentation -- The pole placement method. |
| ctrlnum | (OCoLC)179872855 |
| dewey-full | 629.132/3 |
| dewey-hundreds | 600 - Technology (Applied sciences) |
| dewey-ones | 629 - Other branches of engineering |
| dewey-raw | 629.132/3 |
| dewey-search | 629.132/3 |
| dewey-sort | 3629.132 13 |
| dewey-tens | 620 - Engineering and allied operations |
| discipline | Verkehr / Transport |
| edition | 2nd ed. |
| format | Electronic eBook |
| fullrecord | <?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>05541cam a2200613 a 4500</leader><controlfield tag="001">ZDB-4-EBA-ocn179872855</controlfield><controlfield tag="003">OCoLC</controlfield><controlfield tag="005">20241004212047.0</controlfield><controlfield tag="006">m o d </controlfield><controlfield tag="007">cr cnu---unuuu</controlfield><controlfield tag="008">071030s2007 ne a ob 001 0 eng d</controlfield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">N$T</subfield><subfield code="b">eng</subfield><subfield code="e">pn</subfield><subfield code="c">N$T</subfield><subfield code="d">YDXCP</subfield><subfield code="d">OCLCQ</subfield><subfield code="d">OCLCF</subfield><subfield code="d">OCLCO</subfield><subfield code="d">OCLCQ</subfield><subfield code="d">AGLDB</subfield><subfield code="d">Z5A</subfield><subfield code="d">JBG</subfield><subfield code="d">LIP</subfield><subfield code="d">OCLCQ</subfield><subfield code="d">VTS</subfield><subfield code="d">CEF</subfield><subfield code="d">STF</subfield><subfield code="d">M8D</subfield><subfield code="d">UHL</subfield><subfield code="d">UKAHL</subfield><subfield code="d">OCLCQ</subfield><subfield code="d">OCLCO</subfield><subfield code="d">OCLCQ</subfield><subfield code="d">OCLCO</subfield><subfield code="d">OCLCL</subfield><subfield code="d">OCLCQ</subfield></datafield><datafield tag="019" ind1=" " ind2=" "><subfield code="a">173264081</subfield><subfield code="a">1113311457</subfield></datafield><datafield tag="020" ind1=" " ind2=" "><subfield code="a">9780080550367</subfield><subfield code="q">(electronic bk.)</subfield></datafield><datafield tag="020" ind1=" " ind2=" "><subfield code="a">0080550363</subfield><subfield code="q">(electronic bk.)</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(OCoLC)179872855</subfield><subfield code="z">(OCoLC)173264081</subfield><subfield code="z">(OCoLC)1113311457</subfield></datafield><datafield tag="050" ind1=" " ind2="4"><subfield code="a">TL570</subfield><subfield code="b">.C66 2007eb</subfield></datafield><datafield tag="072" ind1=" " ind2="7"><subfield code="a">TRA</subfield><subfield code="x">002000</subfield><subfield code="2">bisacsh</subfield></datafield><datafield tag="082" ind1="7" ind2=" "><subfield code="a">629.132/3</subfield><subfield code="2">22</subfield></datafield><datafield tag="049" ind1=" " ind2=" "><subfield code="a">MAIN</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Cook, M. V.</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Flight dynamics principles /</subfield><subfield code="c">M.V. Cook.</subfield></datafield><datafield tag="250" ind1=" " ind2=" "><subfield code="a">2nd ed.</subfield></datafield><datafield tag="260" ind1=" " ind2=" "><subfield code="a">Amsterdam ;</subfield><subfield code="a">Boston :</subfield><subfield code="b">Elsevier/Butterworth-Heinemann,</subfield><subfield code="c">2007.</subfield></datafield><datafield tag="300" ind1=" " ind2=" "><subfield code="a">1 online resource (xxi, 468 pages) :</subfield><subfield code="b">illustrations</subfield></datafield><datafield tag="336" ind1=" " ind2=" "><subfield code="a">text</subfield><subfield code="b">txt</subfield><subfield code="2">rdacontent</subfield></datafield><datafield tag="337" ind1=" " ind2=" "><subfield code="a">computer</subfield><subfield code="b">c</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="a">online resource</subfield><subfield code="b">cr</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="490" ind1="1" ind2=" "><subfield code="a">Elsevier aerospace engineering series</subfield></datafield><datafield tag="504" ind1=" " ind2=" "><subfield code="a">Includes bibliographical references and index.</subfield></datafield><datafield tag="588" ind1="0" ind2=" "><subfield code="a">Print version record.</subfield></datafield><datafield tag="505" ind1="0" ind2="0"><subfield code="t">Flight Dynamics Principles --</subfield><subfield code="t">Copyright page --</subfield><subfield code="t">Preface to the first edition --</subfield><subfield code="t">Preface to the second edition --</subfield><subfield code="t">Nomenclature --</subfield><subfield code="g">1.</subfield><subfield code="t">Introduction --</subfield><subfield code="g">1.1.</subfield><subfield code="t">Overview --</subfield><subfield code="g">1.2.</subfield><subfield code="t">Flying and handling qualities --</subfield><subfield code="g">1.3.</subfield><subfield code="t">General considerations --</subfield><subfield code="g">1.4.</subfield><subfield code="t">Aircraft equations of motion --</subfield><subfield code="g">1.5.</subfield><subfield code="t">Aerodynamics --</subfield><subfield code="g">1.6.</subfield><subfield code="t">Computers --</subfield><subfield code="g">1.7.</subfield><subfield code="t">Summary --</subfield><subfield code="g">2.</subfield><subfield code="t">Systems of axes and notation --</subfield><subfield code="g">2.1.</subfield><subfield code="t">Earth axes --</subfield><subfield code="g">2.2.</subfield><subfield code="t">Aircraft body fixed axes --</subfield><subfield code="g">2.3.</subfield><subfield code="t">Euler angles and aircraft attitude --</subfield><subfield code="g">2.4.</subfield><subfield code="t">Axes transformations --</subfield><subfield code="g">2.5.</subfield><subfield code="t">Aircraft reference geometry --</subfield><subfield code="g">2.6.</subfield><subfield code="t">Controls notation --</subfield><subfield code="g">2.7.</subfield><subfield code="t">Aerodynamic reference centres</subfield></datafield><datafield tag="505" ind1="0" ind2="0"><subfield code="g">5.1.</subfield><subfield code="t">Methods of solution --</subfield><subfield code="g">5.2.</subfield><subfield code="t">Cramer's rule --</subfield><subfield code="g">5.3.</subfield><subfield code="t">Aircraft response transfer functions --</subfield><subfield code="g">5.4.</subfield><subfield code="t">Response to controls --</subfield><subfield code="g">5.5.</subfield><subfield code="t">Acceleration response transfer functions --</subfield><subfield code="g">5.6.</subfield><subfield code="t">The state space method --</subfield><subfield code="g">5.7.</subfield><subfield code="t">State space model augmentation --</subfield><subfield code="t">Problems --</subfield><subfield code="g">6.</subfield><subfield code="t">Longitudinal dynamics --</subfield><subfield code="g">6.1.</subfield><subfield code="t">Response to controls --</subfield><subfield code="g">6.2.</subfield><subfield code="t">The dynamic stability modes --</subfield><subfield code="g">6.3.</subfield><subfield code="t">Reduced order models --</subfield><subfield code="g">6.4.</subfield><subfield code="t">Frequency response --</subfield><subfield code="g">6.5.</subfield><subfield code="t">Flying and handling qualities --</subfield><subfield code="g">6.6.</subfield><subfield code="t">Mode excitation --</subfield><subfield code="t">Problems --</subfield><subfield code="g">7.</subfield><subfield code="t">Lateral-directional dynamics --</subfield><subfield code="g">7.1.</subfield><subfield code="t">Response to controls --</subfield><subfield code="g">7.2.</subfield><subfield code="t">The dynamic stability modes --</subfield><subfield code="g">7.3.</subfield><subfield code="t">Reduced order models</subfield></datafield><datafield tag="505" ind1="0" ind2="0"><subfield code="g">7.4.</subfield><subfield code="t">Frequency response --</subfield><subfield code="g">7.5.</subfield><subfield code="t">Flying and handling qualities --</subfield><subfield code="g">7.6.</subfield><subfield code="t">Mode excitation --</subfield><subfield code="t">Problems --</subfield><subfield code="g">8.</subfield><subfield code="t">Manoeuvrability --</subfield><subfield code="g">8.1.</subfield><subfield code="t">Introduction --</subfield><subfield code="g">8.2.</subfield><subfield code="t">The steady pull-up manoeuvre --</subfield><subfield code="g">8.3.</subfield><subfield code="t">The pitching moment equation --</subfield><subfield code="g">8.4.</subfield><subfield code="t">Longitudinal manoeuvre stability --</subfield><subfield code="g">8.5.</subfield><subfield code="t">Aircraft dynamics and manoeuvrability --</subfield><subfield code="g">9.</subfield><subfield code="t">Stability --</subfield><subfield code="g">9.1.</subfield><subfield code="t">Introduction --</subfield><subfield code="g">9.2.</subfield><subfield code="t">The characteristic equation --</subfield><subfield code="g">9.3.</subfield><subfield code="t">The Routh-Hurwitz stability criterion --</subfield><subfield code="g">9.4.</subfield><subfield code="t">The stability quartic --</subfield><subfield code="g">9.5.</subfield><subfield code="t">Graphical interpretation of stability --</subfield><subfield code="t">Problems --</subfield><subfield code="g">10.</subfield><subfield code="t">Flying and handling qualities --</subfield><subfield code="g">10.1.</subfield><subfield code="t">Introduction</subfield></datafield><datafield tag="505" ind1="0" ind2="0"><subfield code="g">10.2.</subfield><subfield code="t">Short term dynamic models --</subfield><subfield code="g">10.3.</subfield><subfield code="t">Flying qualities requirements --</subfield><subfield code="g">10.4.</subfield><subfield code="t">Aircraft role --</subfield><subfield code="g">10.5.</subfield><subfield code="t">Pilot opinion rating --</subfield><subfield code="g">10.6.</subfield><subfield code="t">Longitudinal flying qualities requirements --</subfield><subfield code="g">10.7.</subfield><subfield code="t">Control anticipation parameter --</subfield><subfield code="g">10.8.</subfield><subfield code="t">Lateral-directional flying qualities requirements --</subfield><subfield code="g">10.9.</subfield><subfield code="t">Flying qualities requirements on the s-plane --</subfield><subfield code="t">Problems --</subfield><subfield code="g">11.</subfield><subfield code="t">Stability augmentation --</subfield><subfield code="g">11.1.</subfield><subfield code="t">Introduction --</subfield><subfield code="g">11.2.</subfield><subfield code="t">Augmentation system design --</subfield><subfield code="g">11.3.</subfield><subfield code="t">Closed loop system analysis --</subfield><subfield code="g">11.4.</subfield><subfield code="t">The root locus plot --</subfield><subfield code="g">11.5.</subfield><subfield code="t">Longitudinal stability augmentation --</subfield><subfield code="g">11.6.</subfield><subfield code="t">Lateral-directional stability augmentation --</subfield><subfield code="g">11.7.</subfield><subfield code="t">The pole placement method.</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">The study of flight dynamics requires a thorough understanding of the theory of the stability and control of aircraft, an appreciation of flight control systems and a comprehensive grounding in the theory of automatic control. Flight Dynamics provides all three in an accessible and student focussed text. Written for those coming to the subject for the first time the book is suitable as a complete first course text. It provides a secure foundation from which to move on to more advanced topics such a non-linear flight dynamics, simulation and advanced flight control, and is ideal for tho.</subfield></datafield><datafield tag="650" ind1=" " ind2="0"><subfield code="a">Aerodynamics.</subfield><subfield code="0">http://id.loc.gov/authorities/subjects/sh85001295</subfield></datafield><datafield tag="650" ind1=" " ind2="0"><subfield code="a">Flight control.</subfield><subfield code="0">http://id.loc.gov/authorities/subjects/sh85049111</subfield></datafield><datafield tag="650" ind1=" " ind2="0"><subfield code="a">Stability of airplanes.</subfield><subfield code="0">http://id.loc.gov/authorities/subjects/sh85127186</subfield></datafield><datafield tag="650" ind1=" " ind2="6"><subfield code="a">Aérodynamique.</subfield></datafield><datafield tag="650" ind1=" " ind2="6"><subfield code="a">Systèmes de commande (Vol)</subfield></datafield><datafield tag="650" ind1=" " ind2="6"><subfield code="a">Avions</subfield><subfield code="x">Stabilité.</subfield></datafield><datafield tag="650" ind1=" " ind2="7"><subfield code="a">aerodynamics.</subfield><subfield code="2">aat</subfield></datafield><datafield tag="650" ind1=" " ind2="7"><subfield code="a">TRANSPORTATION</subfield><subfield code="x">Aviation</subfield><subfield code="x">General.</subfield><subfield code="2">bisacsh</subfield></datafield><datafield tag="650" ind1=" " ind2="7"><subfield code="a">Aerodynamics</subfield><subfield code="2">fast</subfield></datafield><datafield tag="650" ind1=" " ind2="7"><subfield code="a">Flight control</subfield><subfield code="2">fast</subfield></datafield><datafield tag="650" ind1=" " ind2="7"><subfield code="a">Stability of airplanes</subfield><subfield code="2">fast</subfield></datafield><datafield tag="776" ind1="0" ind2="8"><subfield code="i">Print version:</subfield><subfield code="a">Cook, M.V.</subfield><subfield code="t">Flight dynamics principles.</subfield><subfield code="b">2nd ed.</subfield><subfield code="d">Amsterdam ; Boston : Elsevier/Butterworth-Heinemann, 2007</subfield><subfield code="z">0750669276</subfield><subfield code="z">9780750669276</subfield><subfield code="w">(OCoLC)171268192</subfield></datafield><datafield tag="830" ind1=" " ind2="0"><subfield code="a">Elsevier aerospace engineering series.</subfield></datafield><datafield tag="856" ind1="4" ind2="0"><subfield code="l">FWS01</subfield><subfield code="p">ZDB-4-EBA</subfield><subfield code="q">FWS_PDA_EBA</subfield><subfield code="u">https://search.ebscohost.com/login.aspx?direct=true&scope=site&db=nlebk&AN=203095</subfield><subfield code="3">Volltext</subfield></datafield><datafield tag="938" ind1=" " ind2=" "><subfield code="a">Askews and Holts Library Services</subfield><subfield code="b">ASKH</subfield><subfield code="n">AH25540755</subfield></datafield><datafield tag="938" ind1=" " ind2=" "><subfield code="a">EBSCOhost</subfield><subfield code="b">EBSC</subfield><subfield code="n">203095</subfield></datafield><datafield tag="938" ind1=" " ind2=" "><subfield code="a">YBP Library Services</subfield><subfield code="b">YANK</subfield><subfield code="n">2703626</subfield></datafield><datafield tag="994" ind1=" " ind2=" "><subfield code="a">92</subfield><subfield code="b">GEBAY</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">ZDB-4-EBA</subfield></datafield><datafield tag="049" ind1=" " ind2=" "><subfield code="a">DE-863</subfield></datafield></record></collection> |
| id | ZDB-4-EBA-ocn179872855 |
| illustrated | Illustrated |
| indexdate | 2024-11-27T13:16:10Z |
| institution | BVB |
| isbn | 9780080550367 0080550363 |
| language | English |
| oclc_num | 179872855 |
| open_access_boolean | |
| owner | MAIN DE-863 DE-BY-FWS |
| owner_facet | MAIN DE-863 DE-BY-FWS |
| physical | 1 online resource (xxi, 468 pages) : illustrations |
| psigel | ZDB-4-EBA |
| publishDate | 2007 |
| publishDateSearch | 2007 |
| publishDateSort | 2007 |
| publisher | Elsevier/Butterworth-Heinemann, |
| record_format | marc |
| series | Elsevier aerospace engineering series. |
| series2 | Elsevier aerospace engineering series |
| spelling | Cook, M. V. Flight dynamics principles / M.V. Cook. 2nd ed. Amsterdam ; Boston : Elsevier/Butterworth-Heinemann, 2007. 1 online resource (xxi, 468 pages) : illustrations text txt rdacontent computer c rdamedia online resource cr rdacarrier Elsevier aerospace engineering series Includes bibliographical references and index. Print version record. Flight Dynamics Principles -- Copyright page -- Preface to the first edition -- Preface to the second edition -- Nomenclature -- 1. Introduction -- 1.1. Overview -- 1.2. Flying and handling qualities -- 1.3. General considerations -- 1.4. Aircraft equations of motion -- 1.5. Aerodynamics -- 1.6. Computers -- 1.7. Summary -- 2. Systems of axes and notation -- 2.1. Earth axes -- 2.2. Aircraft body fixed axes -- 2.3. Euler angles and aircraft attitude -- 2.4. Axes transformations -- 2.5. Aircraft reference geometry -- 2.6. Controls notation -- 2.7. Aerodynamic reference centres 5.1. Methods of solution -- 5.2. Cramer's rule -- 5.3. Aircraft response transfer functions -- 5.4. Response to controls -- 5.5. Acceleration response transfer functions -- 5.6. The state space method -- 5.7. State space model augmentation -- Problems -- 6. Longitudinal dynamics -- 6.1. Response to controls -- 6.2. The dynamic stability modes -- 6.3. Reduced order models -- 6.4. Frequency response -- 6.5. Flying and handling qualities -- 6.6. Mode excitation -- Problems -- 7. Lateral-directional dynamics -- 7.1. Response to controls -- 7.2. The dynamic stability modes -- 7.3. Reduced order models 7.4. Frequency response -- 7.5. Flying and handling qualities -- 7.6. Mode excitation -- Problems -- 8. Manoeuvrability -- 8.1. Introduction -- 8.2. The steady pull-up manoeuvre -- 8.3. The pitching moment equation -- 8.4. Longitudinal manoeuvre stability -- 8.5. Aircraft dynamics and manoeuvrability -- 9. Stability -- 9.1. Introduction -- 9.2. The characteristic equation -- 9.3. The Routh-Hurwitz stability criterion -- 9.4. The stability quartic -- 9.5. Graphical interpretation of stability -- Problems -- 10. Flying and handling qualities -- 10.1. Introduction 10.2. Short term dynamic models -- 10.3. Flying qualities requirements -- 10.4. Aircraft role -- 10.5. Pilot opinion rating -- 10.6. Longitudinal flying qualities requirements -- 10.7. Control anticipation parameter -- 10.8. Lateral-directional flying qualities requirements -- 10.9. Flying qualities requirements on the s-plane -- Problems -- 11. Stability augmentation -- 11.1. Introduction -- 11.2. Augmentation system design -- 11.3. Closed loop system analysis -- 11.4. The root locus plot -- 11.5. Longitudinal stability augmentation -- 11.6. Lateral-directional stability augmentation -- 11.7. The pole placement method. The study of flight dynamics requires a thorough understanding of the theory of the stability and control of aircraft, an appreciation of flight control systems and a comprehensive grounding in the theory of automatic control. Flight Dynamics provides all three in an accessible and student focussed text. Written for those coming to the subject for the first time the book is suitable as a complete first course text. It provides a secure foundation from which to move on to more advanced topics such a non-linear flight dynamics, simulation and advanced flight control, and is ideal for tho. Aerodynamics. http://id.loc.gov/authorities/subjects/sh85001295 Flight control. http://id.loc.gov/authorities/subjects/sh85049111 Stability of airplanes. http://id.loc.gov/authorities/subjects/sh85127186 Aérodynamique. Systèmes de commande (Vol) Avions Stabilité. aerodynamics. aat TRANSPORTATION Aviation General. bisacsh Aerodynamics fast Flight control fast Stability of airplanes fast Print version: Cook, M.V. Flight dynamics principles. 2nd ed. Amsterdam ; Boston : Elsevier/Butterworth-Heinemann, 2007 0750669276 9780750669276 (OCoLC)171268192 Elsevier aerospace engineering series. FWS01 ZDB-4-EBA FWS_PDA_EBA https://search.ebscohost.com/login.aspx?direct=true&scope=site&db=nlebk&AN=203095 Volltext |
| spellingShingle | Cook, M. V. Flight dynamics principles / Elsevier aerospace engineering series. Flight Dynamics Principles -- Copyright page -- Preface to the first edition -- Preface to the second edition -- Nomenclature -- Introduction -- Overview -- Flying and handling qualities -- General considerations -- Aircraft equations of motion -- Aerodynamics -- Computers -- Summary -- Systems of axes and notation -- Earth axes -- Aircraft body fixed axes -- Euler angles and aircraft attitude -- Axes transformations -- Aircraft reference geometry -- Controls notation -- Aerodynamic reference centres Methods of solution -- Cramer's rule -- Aircraft response transfer functions -- Response to controls -- Acceleration response transfer functions -- The state space method -- State space model augmentation -- Problems -- Longitudinal dynamics -- The dynamic stability modes -- Reduced order models -- Frequency response -- Mode excitation -- Lateral-directional dynamics -- Reduced order models Manoeuvrability -- The steady pull-up manoeuvre -- The pitching moment equation -- Longitudinal manoeuvre stability -- Aircraft dynamics and manoeuvrability -- Stability -- The characteristic equation -- The Routh-Hurwitz stability criterion -- The stability quartic -- Graphical interpretation of stability -- Introduction Short term dynamic models -- Flying qualities requirements -- Aircraft role -- Pilot opinion rating -- Longitudinal flying qualities requirements -- Control anticipation parameter -- Lateral-directional flying qualities requirements -- Flying qualities requirements on the s-plane -- Stability augmentation -- Augmentation system design -- Closed loop system analysis -- The root locus plot -- Longitudinal stability augmentation -- Lateral-directional stability augmentation -- The pole placement method. Aerodynamics. http://id.loc.gov/authorities/subjects/sh85001295 Flight control. http://id.loc.gov/authorities/subjects/sh85049111 Stability of airplanes. http://id.loc.gov/authorities/subjects/sh85127186 Aérodynamique. Systèmes de commande (Vol) Avions Stabilité. aerodynamics. aat TRANSPORTATION Aviation General. bisacsh Aerodynamics fast Flight control fast Stability of airplanes fast |
| subject_GND | http://id.loc.gov/authorities/subjects/sh85001295 http://id.loc.gov/authorities/subjects/sh85049111 http://id.loc.gov/authorities/subjects/sh85127186 |
| title | Flight dynamics principles / |
| title_alt | Flight Dynamics Principles -- Copyright page -- Preface to the first edition -- Preface to the second edition -- Nomenclature -- Introduction -- Overview -- Flying and handling qualities -- General considerations -- Aircraft equations of motion -- Aerodynamics -- Computers -- Summary -- Systems of axes and notation -- Earth axes -- Aircraft body fixed axes -- Euler angles and aircraft attitude -- Axes transformations -- Aircraft reference geometry -- Controls notation -- Aerodynamic reference centres Methods of solution -- Cramer's rule -- Aircraft response transfer functions -- Response to controls -- Acceleration response transfer functions -- The state space method -- State space model augmentation -- Problems -- Longitudinal dynamics -- The dynamic stability modes -- Reduced order models -- Frequency response -- Mode excitation -- Lateral-directional dynamics -- Reduced order models Manoeuvrability -- The steady pull-up manoeuvre -- The pitching moment equation -- Longitudinal manoeuvre stability -- Aircraft dynamics and manoeuvrability -- Stability -- The characteristic equation -- The Routh-Hurwitz stability criterion -- The stability quartic -- Graphical interpretation of stability -- Introduction Short term dynamic models -- Flying qualities requirements -- Aircraft role -- Pilot opinion rating -- Longitudinal flying qualities requirements -- Control anticipation parameter -- Lateral-directional flying qualities requirements -- Flying qualities requirements on the s-plane -- Stability augmentation -- Augmentation system design -- Closed loop system analysis -- The root locus plot -- Longitudinal stability augmentation -- Lateral-directional stability augmentation -- The pole placement method. |
| title_auth | Flight dynamics principles / |
| title_exact_search | Flight dynamics principles / |
| title_full | Flight dynamics principles / M.V. Cook. |
| title_fullStr | Flight dynamics principles / M.V. Cook. |
| title_full_unstemmed | Flight dynamics principles / M.V. Cook. |
| title_short | Flight dynamics principles / |
| title_sort | flight dynamics principles |
| topic | Aerodynamics. http://id.loc.gov/authorities/subjects/sh85001295 Flight control. http://id.loc.gov/authorities/subjects/sh85049111 Stability of airplanes. http://id.loc.gov/authorities/subjects/sh85127186 Aérodynamique. Systèmes de commande (Vol) Avions Stabilité. aerodynamics. aat TRANSPORTATION Aviation General. bisacsh Aerodynamics fast Flight control fast Stability of airplanes fast |
| topic_facet | Aerodynamics. Flight control. Stability of airplanes. Aérodynamique. Systèmes de commande (Vol) Avions Stabilité. aerodynamics. TRANSPORTATION Aviation General. Aerodynamics Flight control Stability of airplanes |
| url | https://search.ebscohost.com/login.aspx?direct=true&scope=site&db=nlebk&AN=203095 |
| work_keys_str_mv | AT cookmv flightdynamicsprinciples |