Space Vehicle Dynamics and Control, Second Edition | by Bong Wie | ISBN: 9781563479533. Dynamic Systems Control. Attitude and Orbit Control of Space Solar Power Satellites. Orbital Dynamics and Control. Orbital Maneuvers and Control. Attitude Dynamics and Control. Rotational Maneuvers and Attitude Control.

March 12th, 2010 | by kutenk |

Space Vehicle Dynamics and Control, Second Edition

by Bong Wie
ISBN:9781563479533

Requiring knowledge of vector and matrix algebra, calculus, ordinary differential equations, engineering mechanics, and linear system dynamics and control, this book provides a solid foundation in dynamic modeling, analysis, and control of space vehicles.

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Space Vehicle Dynamics and Control, Second Edition







Foreword
Preface to the Second Edition
Preface to the First Edition
Part 1 – Dynamic Systems Modeling, Analysis, and Control
Chapter 1 – Dynamic Systems Modeling and Analysis
1.1: Matrix and Vector Analysis
1.2: Classical Mechanics
1.3: Dynamic Systems Analysis
References




Chapter 2 – Dynamic Systems Control
2.1: Feedback Control Systems
2.2: Classical Frequency-Domain Methods
2.3: Classical Gain-Phase Stabilization
2.4: Digital Control
2.5: Modern State-Space Methods
2.6: Stability Robustness Analysis
2.7: Robust Control of Uncertain Dynamic Systems
References

Part 2 – Orbital Dynamics and Control
Chapter 3 – Orbital Dynamics
Overview
3.1: Two-Body Problem
3.2: Geometry of Conic Sections
3.3: Vis-Viva Equation
3.4: Kepler’s Time Equation
3.5: Orbital Position and Velocity
3.6: Orbital Perturbations
3.7: Circular Restricted Three-Body Problem
3.8: Elliptic Restricted Three-Body Problem
References

Chapter 4 – Orbital Maneuvers and Control
4.1: Launch Vehicle Trajectories
4.2: Orbit Injection
4.3: Single-Impulse Maneuvers
4.4: Hohmann Transfer
4.5: Interplanetary Flight
4.6: Orbital Rendezvous
4.7: Halo Orbit Determination and Control
References

Part 3 – Attitude Dynamics and Control
Chapter 5 – Rotational Kinematics
5.1: Direction Cosine Matrix
5.2: Euler Angles
5.3: Euler’s Eigenaxis Rotation
5.4: Quaternions
5.5: Kinematic Differential Equations
References

Chapter 6 – Rigid-Body Dynamics
6.1: Angular Momentum of a Rigid Body
6.2: Inertia Matrix and Inertia Dyadic
6.3: Principal Axes
6.4: Euler’s Rotational Equations of Motion
6.5: Torque-Free Motion of an Axisymmetric Rigid Body
6.6: General Torque-Free Motion
6.7: Stability of Torque-Free Motion About Principal Axes
6.8: Spinning Axisymmetric Body with Constant Body-Fixed Torque
6.9: Asymmetric Rigid Body with Constant Body-Fixed Torques
6.10: Rigid Body in a Circular Orbit
6.11: Gyrostat in a Circular Orbit
6.12: Dual-Spinner with a Platform Damper
References




Chapter 7 – Rotational Maneuvers and Attitude Control
7.1: Control of Spinning Spacecraft
7.2: Time-Optimal Reorientation Maneuvers
7.3: Quaternion-Feedback Reorientation Maneuvers
7.4: Attitude Control and Momentum Management
7.5: Steering Logic for Control Moment Gyros
7.6: Optimal Jet Selection Logic
7.7: Pulse-Modulated Attitude Control
References

Part 4 – Structural Dynamics and Control
Chapter 8 – Structural Dynamics
8.1: Introduction
8.2: Uniform Bars
8.3: Uniform Beams
8.4: Rigid Body with Beamlike Appendages
8.5: Rigid/Flexible Frame with a Pretensioned Membrane
8.6: Flexible Toroidal Structures
8.7: Summary
References

Chapter 9 – Attitude and Structural Control
9.1: Thrust Vector Control Design for a Spacecraft with Propellant Sloshing
9.2: Attitude Control Design for a Bias-Momentum Stabilized Spacecraft
9.3: Stationkeeping Attitude Control of a Flexible Spacecraft
9.4: Nonlinear Pulse-Modulated Control Analysis and Design
9.5: Attitude Control Redesign for the Hubble Space Telescope
9.6: Active Structural Vibration Control
9.7: Summary
References

Chapter 10 – Robust Optimal Maneuvers
10.1: Time-Optimal Control
10.2: Robust Time-Optimal Control
10.3: Robust Time-Optimal Control Using One-Sided Control Inputs
10.4: Robust Fuel- and Time-Optimal Control
10.5: Robustified Feedforward and Feedback Control
References

Part 5 – Advanced Spacecraft Dynamics and Control
Chapter 11 – Control Moment Gyros for Agile Imaging Satellites
11.1: Introduction
11.2: Single-Gimbal CMG Systems
11.3: CMG Singularities and Singular Surfaces
11.4: Singularity Analysis Using the Binet—Cauchy Identity
11.5: CMG Null Motions
11.6: Surface Theory of Differential Geometry
11.7: Singularity-Robust Steering Logic
11.8: Singularity Avoidance/Escape Logic
11.9: Rapid Multitarget Acquisition and Pointing Control of Agile Spacecraft
11.10: Variable-Speed Control Moment Gyros
References

Chapter 12 – Solar-Sail Dynamics and Control
12.1: Introduction
12.2: Solar-Sail Attitude Control Issues
12.3: Solar-Radiation-Pressure Models
12.4: Spin Stabilization of Sailcraft
12.5: Sailcraft in an Earth-Centered Elliptic Orbit
12.6: Solar-Sail Attitude Control Using a Gimbaled Control Boom and Control Vanes
12.7: Gimbaled Thrust Vector Control Design for a Sailcraft
12.8: Attitude Control System Architecture for Solar Sails
12.9: Solar-Sail Flight Validation (SSFV) Mission
12.10: Attitude Dynamics of a Solar Sail with Translating Control Masses
12.11: Preliminary Design of the Propellantless Primary ACS
12.12: Micro-PPT-Based Secondary ACS for Solar Sails
12.13: Orbital Dynamics of Solar Sails
12.14: Examples of Solar-Sail Trajectory Design
12.15: Solar-Sail Thrust Vector Control Design
12.16: TVC Design and Simulation for the SPI Mission
12.17: Attitude Control of a Solar Sail in Sun-Synchronous Orbit Using Reaction Wheels and Magnetic Torquers
References




Chapter 13 – Solar-Sail Missions for Asteroid Deflection
13.1: Introduction to the NEO Deflection Problem
13.2: Solar-Sail Mission Concept for Asteroid Deflection
13.3: Asteroid Deflection Using a Gravity Tractor
13.4: Multiple Gravity Tractors in Halo Orbits
13.5: Hovering Solar-Sail Gravity Tractor
13.6: Asteroid Deflection Dynamics
References

Chapter 14 – Attitude and Orbit Control of Space Solar Power Satellites
14.1: Introduction
14.2: System Description
14.3: Orbital Dynamics
14.4: Attitude Motion of an Inertially Oriented Spacecraft
14.5: Structural Control Issues
14.6: Attitude and Orbit Control
14.7: Summary
References

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