Advanced Control of Aircraft, Spacecraft and Rockets

Name: Advanced Control of Aircraft, Spacecraft and Rockets
Price: 33.91 USD
Availability: InStock
ISBN: 9780470745632

ISBN-10: 0470745630

ISBN-13: 9780470745632

Edition: 2011

Authors: Doug Marschke, Harry Reynolds, Ashish Tewari

List price: $66.50

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Description:

Advanced Control of Aircraft, Missiles and Spacecraft introduces the reader to the concepts of modern control theory applied to the design and analysis of general flight control systems in a concise and mathematically rigorous style. It presents a comprehensive treatment of both atmospheric and space flight control systems including aircraft, rockets (missiles and launch vehicles), entry vehicles and spacecraft (both orbital and attitude control). The broad coverage of topics emphasizes the synergies among the various flight control systems and attempts to show their evolution from the same set of physical principles as well as their design and analysis by similar mathematical tools. In…

Book details

List price: $66.50
Copyright year: 2011
Publisher: John Wiley & Sons, Limited
Publication date: 7/1/2011
Binding: Hardcover
Pages: 454
Size: 7.00" wide x 10.00" long x 1.00" tall
Weight: 2.046
Language: English

Doug Marschke is an engineering graduate from the University of Michigan currently working with various consulting firms, including Strategic and Cubed networks. He is JNCIE-ER #3, JNCIE-M #41, and JNCIS-FW certified. He was heavily involved in the Juniper certification exams from the start, having contributed to test writing, and is a coauthor of the current JNCIE Enterprise Exam. Doug currently spends his time working with both service providers and enterprises to optimize their IP networks for better performance, cost, and reliability. He also flies around the world sharing his knowledge in a variety of training classes and seminars with topics ranging from troubleshooting to design and…

Harry Reynolds has over twenty-five years experience in the networking industry, with the last fifteen years focused on LANs and LAN interconnection. He is CCIE # 4977, and JNCIE # 3, and also holds various other industry and teaching certifications. Harry was a contributing author on the Juniper Network Complete Reference (McGraw- Hill, 2002), and wrote the JNCIE and JNCIP Study Guides for (Sybex Books 2003). Prior to joining Juniper, Harry had served time in the US Navy as an Avionics Technician, worked for equipment manufacturer Micom Systems, and spent much time developing and presenting hands-on technical training curriculums targeted to both enterprise and service provider needs.…



Series


Preface


Preface



Introduction



Notation and Basic Definitions



Control Systems



Linear Tracking Systems



Linear Time-Invariant Tracking Systems



Guidance and Control of Flight Vehicles



Special Tracking Laws



Proportional Navigation Guidance



Cross-Product Steering



Proportional-Integral-Derivative Control



Digital Tracking System



Summary


Exercises


References



Optimal Control Techniques



Introduction



Multi-variable Optimization



Constrained Minimization



Equality Constraints



Inequality Constraints



Optimal Control of Dynamic Systems



Optimality Conditions



The Hamiltonian and the Minimum Principle



Hamilton–Jacobi–Bellman Equation



Linear Time-Varying System with Quadratic Performance Index



Optimal Control with End-Point State Equality Constraints



Euler–Lagrange Equations



Special Cases



Numerical Solution of Two-Point Boundary Value Problems



Shooting Method



Collocation Method



Optimal Terminal Control with Interior Time Constraints



Optimal Singular Control



Tracking Control



Neighboring Extremal Method and Linear Quadratic Control



Stochastic Processes



Stationary Random Processes



Filtering of Random Noise



Kalman Filter



Robust Linear Time-Invariant Control



LQG/LTR Method



H2/H E E Design Methods



Summary


Exercises


References



Optimal Navigation and Control of Aircraft



Aircraft Navigation Plant



Wind Speed and Direction



Navigational Subsystems



Optimal Aircraft Navigation



Optimal Navigation Formulation



Extremal Solution of the Boundary-Value Problem: Long-Range Flight Example



Great Circle Navigation



Aircraft Attitude Dynamics



Translational and Rotational Kinetics



Attitude Relative to the Velocity Vector



Aerodynamic Forces and Moments



Longitudinal Dynamics



Longitudinal Dynamics Plant



Optimal Multi-variable Longitudinal Control



Multi-input Optimal Longitudinal Control



Optimal Airspeed Control



LQG/LTR Design Example



H E E Design Example



Altitude and Mach Control



Lateral-Directional Control Systems



Lateral-Directional Plant



Optimal Roll Control



Multi-variable Lateral-Directional Control: Heading-Hold Autopilot



Optimal Control of Inertia-Coupled Aircraft Rotation



Summary


Exercises


References



Optimal Guidance of Rockets



Introduction



Optimal Terminal Guidance of Interceptors



Non-planar Optimal Tracking System for Interceptors: 3DPN



Flight in a Vertical Plane



Optimal Terminal Guidance



Vertical Launch of a Rocket (Goddard’s Problem)



Gravity-Turn Trajectory of Launch Vehicles



Launch to Circular Orbit: Modulated Acceleration



Launch to Circular Orbit: Constant Acceleration



Launch of Ballistic Missiles



Gravity-Turn with Modulated Forward Acceleration



Modulated Forward and Normal Acceleration



Planar Tracking Guidance System



Stability, Controllability, and Observability



Nominal Plant for Tracking Gravity-Turn Trajectory



Robust and Adaptive Guidance



Guidance with State Feedback



Guidance with Normal Acceleration Input



Observer-Based Guidance of Gravity-Turn Launch Vehicle



Altitude-Based Observer with Normal Acceleration Input



Bi-output Observer with Normal Acceleration Input



Mass and Atmospheric Drag Modeling



Summary


Exercises


References



Attitude Control of Rockets



Introduction



Attitude Control Plant



Closed-Loop Attitude Control



Roll Control System



Pitch Control of Rockets



Pitch Program



Pitch Guidance and Control System



Adaptive Pitch Control System



Yaw Control of Rockets



Summary 295 Exercises


Reference



Spacecraft Guidance Systems



Introduction



Orbital Mechanics



Orbit Equation



Perifocal and Celestial Frames



Time Equation



Lagrange’s Coefficients



Spacecraft Terminal Guidance



Minimum Energy Orbital Transfer



Lambert’s Theorem



Lambert’s Problem



Lambert Guidance of Rockets



Optimal Terminal Guidance of Re-entry Vehicles



General Orbital Plant for Tracking Guidance



Planar Orbital Regulation



Optimal Non-planar Orbital Regulation



Summary


Exercises


References



Optimal Spacecraft Attitude Control



Introduction



Terminal Control of Spacecraft Attitude



Optimal Single-Axis Rotation of Spacecraft



Multi-axis Rotational Maneuvers of Spacecraft



Spacecraft Control Torques



Rocket Thrusters



Reaction Wheels, Momentum Wheels and Control Moment Gyros



Magnetic Field Torque



Satellite Dynamics Plant for Tracking Control



Environmental Torques



Gravity-Gradient Torque



Multi-variable Tracking Control of Spacecraft Attitude



Active Attitude Control of Spacecraft by Reaction Wheels



Summary


Exercises


References



Linear Systems



Definition



Linearization



Solution to Linear State Equations



Homogeneous Solution



General Solution



Linear Time-Invariant System



Linear Time-Invariant Stability Criteria



Controllability of Linear Time-Invariant Systems



Observability of Linear Time-Invariant Systems



Transfer Matrix



Singular Value Decomposition



Linear Time-Invariant Control Design



Regulator Design by Eigenstructure Assignment



Regulator Design by Linear Optimal Control



Linear Observers and Output Feedback Compensators


References



Stability



Preliminaries



Stability in the Sense of Lagrange



Stability in the Sense of Lyapunov



Asymptotic Stability



Global Asymptotic Stability



Lyapunov’s Theorem



Krasovski’s Theorem



Lyapunov Stability of Linear Systems


References



Control of Underactuated Flight Systems



Adaptive Rocket Guidance with Forward Acceleration Input



Thrust Saturation and Rate Limits (Increased Underactuation)



Single- and Bi-output Observers with Forward Acceleration Input


References


Index