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001 ocn923345221
003 OCoLC
005 20220908100047.0
006 m o d
007 cr |n|||||||||
008 151009s1994 nju ob 001 0 eng d
040 _aIDEBK
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019 _a946713568
_a949649603
_a992906246
_a999371744
_a1002232439
_a1004874642
_a1066441083
020 _a1400880033
_q(electronic bk.)
020 _a9781400880034
_q(electronic bk.)
020 _a9781680159295
_q(electronic bk.)
020 _a1680159291
_q(electronic bk.)
020 _a9780691087825
_q(alk. paper)
020 _a0691087822
_q(alk. paper)
029 1 _aAU@
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029 1 _aDEBBG
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029 1 _aGBVCP
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035 _a(OCoLC)923345221
_z(OCoLC)946713568
_z(OCoLC)949649603
_z(OCoLC)992906246
_z(OCoLC)999371744
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037 _a834876
_bMIL
037 _a22573/ctt17kmrfc
_bJSTOR
037 _a9453456
_bIEEE
050 4 _aTL3260
_b.B78 1994
072 7 _aTEC
_x009000
_2bisacsh
072 7 _aTEC002000
_2bisacsh
082 0 4 _a629.45
_223
084 _aZO 7230
_2rvk
049 _aMAIN
100 1 _aBryson, Arthur E.
_q(Arthur Earl)
_964420
245 1 0 _aControl of spacecraft and aircraft /
_cArthur E. Bryson, Jr.
260 _aPrinceton, N.J. :
_bPrinceton University Press,
_c�1994.
300 _a1 online resource
336 _atext
_btxt
_2rdacontent
337 _acomputer
_bc
_2rdamedia
338 _aonline resource
_bcr
_2rdacarrier
347 _adata file
_2rda
588 0 _aOnline resource; title from PDF title page (EBSCO, viewed October 20, 2015).
504 _aIncludes bibliographical references and index.
520 _aHere a leading researcher provides a comprehensive treatment of the design of automatic control logic for spacecraft and aircraft. In this book author describes the linear-quadratic-regulator (LQR) method of feedback control synthesis, which coordinates multiple controls, producing graceful maneuvers comparable to those of an expert pilot. The first half of the work is about attitude control of rigid and flexible spacecraft using momentum wheels, spin, fixed thrusters, and gimbaled engines. Guidance for nearly circular orbits is discussed. The second half is about aircraft attitude and flight path control. This section discusses autopilot designs for cruise, climb-descent, coordinated turns, and automatic landing. One chapter deals with controlling helicopters near hover, and another offers an introduction to the stabilization of aeroelastic instabilities. --
_cProvided by publisher.
505 0 _aCover; Title; Copyright; Dedication; Contents; List of Figures; List of Tables; Preface and Acknowledgments; Chapter 1 -- Natural Motions of Rigid Spacecraft; 1.1 Translational Motions in Space; 1.2 Translational Motions in Circular Orbit; 1.3 Rotational Motions in Space; 1.4 Rotational Motions in Circular Orbit; 1.5 Disturbances; Chapter 2 -- Spacecraft Sensors and Attitude Determination; 2.1 Introduction; 2.2 Infra-Red, Optical, and Radar Sensors; 2.3 Orbital Gyrocompassing; 2.4 Gyros; 2.5 Inertial Measurement Units; Chapter 3 -- Attitude Control with Thrusters.
505 8 _a3.1 Fast versus Slow Attitude Control3.2 Fast Attitude Control Using Proportional Thrusters; 3.3 Fast Attitude Control Using On-Off Thrusters; Chapter 4 -- Attitude Control with Reaction Wheels; 4.1 Fast Control; 4.2 Slow Pitch Control Using Gravity Desaturation; 4.3 Slow Roll/Yaw Control Using Gravity Desaturation; Chapter 5 -- Attitude Stabilization with Spin; 5.1 Spin Stabilization; 5.2 Nutation Damping; 5.3 Dual Spin; 5.4 Offset Axial Thruster; Chapter 6 -- Attitude Control with a Gimbaled Momentum Wheel; 6.1 Introduction; 6.2 Fast Control; 6.3 Slow Control Using Gravity Desaturation.
505 8 _aChapter 7 -- Attitude Control during Thrust Maneuvers7.1 Using Reaction Jets; 7.2 Using a Gimbaled Engine; 7.3 Using Off-Modulation or Spin; Chapter 8 -- Control of Translational Motions; 8.1 Fast Control; 8.2 Slow Control in Nearly Circular Orbit; Cross Track; 8.3 Slow Control in Circular Orbit; In-Track/Radial; Chapter 9 -- Flexibility and Fuel Slosh; 9.1 Introduction; 9.2 Control Synthesis Using One Vibration Mode; 9.3 Parasitic Modes; 9.4 Control with Fuel Slosh; 9.5 Robust Compensator Synthesis; Chapter 10 -- Natural Motions of Rigid Aircraft; 10.1 Equations of Motion.
505 8 _a10.2 Natural Longitudinal Motions10.3 Natural Lateral Motions; 10.4 Wind Disturbances; Chapter 11 -- Aircraft Sensors; 11.1 Introduction; 11.2 Vertical Gyros; 11.3 Directional Gyros; 11.4 Inertial Measurement Units; 11.5 Baro-Inertial Altimeters; Chapter 12 -- Control of Longitudinal Motions of Aircraft; 12.1 Introduction; 12.2 Steady-State Control; 12.3 Observability and Controllability; 12.4 Control of Climb Rate and Airspeed; 12.5 Control of Altitude and Airspeed; 12.6 Glide-Slope Capture and Hold; 12.7 Flare; Chapter 13 -- Control of Lateral Motions of Aircraft; 13.1 Introduction.
505 8 _a13.2 Steady Bank Angle and Lateral Specific Force13.3 Steady Sideslip and Yaw Rate; 13.4 Observability and Controllability of Lateral Modes; 13.5 Control of Bank Angle and Sideforce; 13.6 Control of Heading and Sideforce; 13.7 Control of Track and Sideforce; Chapter 14 -- Control of Helicopters near Hover; 14.1 Introduction; 14.2 Small Deviations from Steady Hover; 14.3 Steady-State Control near Hover; 14.4 Control of Velocity Vector and Yaw Rate; Chapter 15 -- Aeroelastic Systems; 15.1 Introduction; 15.2 A Simple System with a Flutter Mode; 15.3 Flutter Suppression for a Simple System.
505 8 _aAppendix A -- Linear System Representations.
590 _aIEEE
_bIEEE Xplore Princeton University Press eBooks Library
650 0 _aSpace vehicles
_xAttitude control systems.
_964421
650 0 _aAirplanes
_xControl systems.
_964422
650 6 _aV�ehicules spatiaux
_xSyst�emes de commande d'orientation.
_964423
650 6 _aAvions
_xSyst�emes de commande.
_964424
650 7 _aTECHNOLOGY & ENGINEERING
_xEngineering (General)
_2bisacsh
_94639
650 7 _aTECHNOLOGY & ENGINEERING
_xAeronautics & Astronautics.
_2bisacsh
_964203
650 7 _aAirplanes
_xControl systems.
_2fast
_0(OCoLC)fst00803111
_964422
650 7 _aSpace vehicles
_xAttitude control systems.
_2fast
_0(OCoLC)fst01127962
_964421
650 7 _aFlugregler
_2gnd
_964425
650 7 _aFlugzeug
_2gnd
_964426
650 7 _aFlugregelung
_2gnd
_964427
655 0 _aElectronic book.
_97794
655 4 _aElectronic books.
_93294
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938 _aAskews and Holts Library Services
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938 _aDe Gruyter
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938 _aProQuest Ebook Central
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938 _aEBSCOhost
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938 _aProQuest MyiLibrary Digital eBook Collection
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