Text| Item type | Current library | Collection | Call number | URL | Status | Date due | Barcode | |
|---|---|---|---|---|---|---|---|---|
Reference Book
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Amity Central Library ASET Aerospace | Reference | 629.11 TEW-A (Browse shelf(Opens below)) | Link to resource | Not For Loan | 29315 | ||
Books
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Amity Central Library ASET Aerospace | 629.11 TEW-A (Browse shelf(Opens below)) | Link to resource | Available | 29316 |
1 Introduction
1.1 Notation and Basic Definitions
1.2 Control Systems
1.3 Guidance and Control of Flight Vehicles
1.4 Special Tracking Laws
1.5 Digital Tracking System
1.6 Summary
2 Optimal Control Techniques
2.1 Introduction
2.2 Multi-variable Optimization
2.3 Constrained Minimization
2.4 Optimal Control of Dynamic Systems
2.5 The Hamiltonian and the Minimum Principle
2.6 Optimal Control with End-Point State Equality Constraints
2.7 Numerical Solution of Two-Point Boundary Value Problems
2.8 Optimal Terminal Control with Interior Time Constraints
2.9 Tracking Control
2.10 Stochastic Processes
2.11 Kalman Filter
2.12 Robust Linear Time-Invariant Control
2.13 Summary
3 Optimal Navigation and Control of Aircraft
3.1 Aircraft Navigation Plant
3.2 Optimal Aircraft Navigation
3.3 Aircraft Attitude Dynamics
3.4 Aerodynamic Forces and Moments
3.5 Longitudinal Dynamics
3.6 Optimal Multi-variable Longitudinal Control
3.7 Multi-input Optimal Longitudinal Control
3.8 Optimal Airspeed Control
3.9 Lateral-Directional Control Systems
3.10 Optimal Control of Inertia-Coupled Aircraft Rotation
3.11 Summary
4 Optimal Guidance of Rockets
4.1 Introduction
4.2 Optimal Terminal Guidance of Interceptors
4.3 Non-planar Optimal Tracking System for Interceptors: 3DPN
4.4 Flight in a Vertical Plane
4.5 Optimal Terminal Guidance
4.6 Vertical Launch of a Rocket (Goddard's Problem)
4.7 Gravity-Turn Trajectory of Launch Vehicles
4.8 Launch of Ballistic Missiles
4.9 Planar Tracking Guidance System
4.10 Robust and Adaptive Guidance
4.11 Guidance with State Feedback
4.12 Observer-Based Guidance of Gravity-Turn Launch Vehicle
4.13 Mass and Atmospheric Drag Modeling
4.14 Summary
5 Attitude Control of Rockets
5.1 Introduction
5.2 Attitude Control Plant
5.3 Closed-Loop Attitude Control
5.4 Roll Control System
5.5 Pitch Control of Rockets
5.6 Yaw Control of Rockets
5.7 Summary
6 Spacecraft Guidance Systems
6.1 Introduction
6.2 Orbital Mechanics
6.3 Spacecraft Terminal Guidance
6.4 General Orbital Plant for Tracking Guidance
6.5 Planar Orbital Regulation
6.6 Optimal Non-planar Orbital Regulation
6.7 Summary
7 Optimal Spacecraft Attitude Control
7.1 Introduction
7.2 Terminal Control of Spacecraft Attitude
7.3 Multi-axis Rotational Maneuvers of Spacecraft
7.4 Spacecraft Control Torques
7.5 Satellite Dynamics Plant for Tracking Control
7.6 Environmental Torques
7.7 Multi-variable Tracking Control of Spacecraft Attitude
7.8 Summary
Appendix A: Linear Systems
A.1 Definition
A.2 Linearization
A.3 Solution to Linear State Equations
A.4 Linear Time-Invariant System
A.5 Linear Time-Invariant Stability Criteria
A.6 Controllability of Linear Time-Invariant Systems
A.7 Observability of Linear Time-Invariant Systems
A.8 Transfer Matrix
A.9 Singular Value Decomposition
A.10 Linear Time-Invariant Control Design
Appendix B: Stability
B.1 Preliminaries
B.2 Stability in the Sense of Lagrange
B.3 Stability in the Sense of Lyapunov
Appendix C: Control of Underactuated Flight Systems
C.1 Adaptive Rocket Guidance with Forward Acceleration Input
C.2 Thrust Saturation and Rate Limits (Increased Underactuation)
C.3 Single- and Bi-output Observers with Forward Acceleration Input
References
Index
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