Control of Spacecraft and Aircraft /

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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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Detalles Bibliográficos
Autor principal: Bryson, Arthur E. (Arthur Earl)
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Princeton, N.J. : Princeton University Press, 1994.
Colección:Book collections on Project MUSE.
Temas:
Flugregelung
Flugzeug
Flugregler
Space vehicles > Attitude control systems.
Airplanes > Control systems.
TECHNOLOGY & ENGINEERING > Aeronautics & Astronautics.
TECHNOLOGY & ENGINEERING > Engineering (General)
Avions > Systemes de commande.
Vehicules spatiaux > Systemes de commande d'orientation.
Electronic book.
Electronic books.
Acceso en línea:Texto completo
Tabla de Contenidos:
  • 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.
  • 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.
  • 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.
  • 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.
  • 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.
  • Appendix A
  • Linear System Representations.

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