Control of spacecraft and aircraft

Here 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 maneuver...

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Bibliographic Details
Main Author: Bryson, Arthur E.
Format: eBook
Language: English
Published: Princeton, N.J. : Princeton University Press, ©1994.
Subjects:
Space vehicles > Attitude control systems.
Airplanes > Control systems.
elektronické knihy
electronic books
ISBN: 1400880033
9781400880034
9781680159295
1680159291
9780691087825
0691087822
Physical Description: 1 online resource

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Table of contents

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008 151009s1994 nju ob 001 0 eng d
040 |a IDEBK  |b eng  |e pn  |c IDEBK  |d N$T  |d OCLCF  |d JSTOR  |d KNOVL  |d EBLCP  |d OCLCQ  |d YDXCP  |d COO  |d DEBBG  |d ZCU  |d OCLCQ  |d HEBIS  |d DEGRU  |d IOG  |d EZ9  |d DKU  |d CEF  |d RRP  |d OCLCQ  |d TXC  |d AU@  |d WYU  |d LVT  |d OCLCQ  |d UKAHL  |d OCLCQ  |d ERF  |d OCLCQ  |d AUD  |d S2H  |d OCLCO  |d IEEEE  |d OCLCO  |d OCLCQ  |d OCLCO  |d OCLCL  |d OCLCQ  |d SXB 
020 |a 1400880033  |q (electronic bk.) 
020 |a 9781400880034  |q (electronic bk.) 
020 |a 9781680159295  |q (electronic bk.) 
020 |a 1680159291  |q (electronic bk.) 
020 |a 9780691087825  |q (alk. paper) 
020 |a 0691087822  |q (alk. paper) 
035 |a (OCoLC)923345221  |z (OCoLC)946713568  |z (OCoLC)949649603  |z (OCoLC)992906246  |z (OCoLC)999371744  |z (OCoLC)1002232439  |z (OCoLC)1004874642  |z (OCoLC)1066441083 
100 1 |a Bryson, Arthur E.  |q (Arthur Earl)  |1 https://id.oclc.org/worldcat/entity/E39PBJfh7HvTP3Y8HQHqqQFh73 
245 1 0 |a Control of spacecraft and aircraft /  |c Arthur E. Bryson, Jr. 
260 |a Princeton, N.J. :  |b Princeton University Press,  |c ©1994. 
300 |a 1 online resource 
336 |a text  |b txt  |2 rdacontent 
337 |a computer  |b c  |2 rdamedia 
338 |a online resource  |b cr  |2 rdacarrier 
504 |a Includes bibliographical references and index. 
506 |a Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty 
520 |a Here 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. --  |c Provided by publisher. 
505 0 |a Cover; 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 |a 3.1 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 |a Chapter 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 |a 10.2 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 |a 13.2 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 |a Appendix A -- Linear System Representations. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Space vehicles  |x Attitude control systems. 
650 0 |a Airplanes  |x Control systems. 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpCSA00002/control-of-spacecraft?kpromoter=marc  |y Full text 

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