This chapter contains sections titled:
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 of Ballistic Missiles
Planar Tracking Guidance System
Robust and Adaptive Guidance
Guidance with State Feedback
Observer‐Based Guidance of Gravity‐Turn Launch Vehicle
Mass and Atmospheric Drag Modeling
Summary
Exercises
References
Optimal Guidance of Rockets
2011-07-15
81 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
optimal guidance of rockets ‐ time‐varying parameters, of equations of motion , 3DPN guidance system ‐ and inertia dynamics, feedforward reference input , fast response times ‐ in translation and rotation of rockets , rockets, as gravity‐turn launch vehicles ‐ and short‐range missiles , rocket guidance, three‐dimensional terminal guidance ‐ maneuvering target interception , optimal terminal guidance ‐ optimal control with end‐point constraints , translational motion of center of mass ‐ of flight vehicle, in vertical plane , vertical launch of a rocket (Goddard's Problem) ‐ rocket flight for a vertical launch , ballistic missile launch ‐ guiding a gravity‐turn rocket , robust and adaptive guidance ‐ changing trajectory of a rocket, precluding real‐time computation by linear time‐invariant (LTI) approximation
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