Astrodynamics-optimization theory and guidance theory Research achievements review series no. 15-16
Review of research achievements in astrodynamics, optimization theory, and guidance theory
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Review of research achievements in astrodynamics, optimization theory, and guidance theory
Trajectory physics optimization for boundary value problem solution
Introduction to research achievements review in astrodynamics, optimization theory, and guidance theory
Optimization theory and converse of circle criterion for simple time-varying feedback system
Time-optimal control theory applied to launch vehicle regulation and the newton-raphson optimization method
Optimal control problems solved by application of differential game theory
Let V(t) be a vector-valued function for t belonging to closed interval a,b open interval, a real interval. The main purpose of this paper is to establish the existence of a closed interval alpha,beta contained in closed interval a,b for which there exists a t(sub O) belonging to closed interval alpha,beta contained in closed interval a,b such that V(t(sub O)) = 0, the zero vector. Use of such information in the dynamic optimization theory with multiple objectives present is needed. Examples of such systems will be given.
Energy and accuracy factors in feedback path control system design for optimizing space shuttle trajectory control at subsonic speed
In this paper, step-by-step procedures of applying the H-infinity theory to robust control systems design are given. The objective of the paper is to eliminate the possible difficulties a control engineer may encounter in applying H-infinity control theory and to clear up some misconceptions about H-infinity theory like high-gain controller and numerical obstacles, etc. An efficient algorithm is used to compute the optimal H-infinity norm. The Glover and Doyle (1988) controller formulas are slightly modified and used to construct an optimal controller without any numerical difficulties.
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Optimal guidance approximations using perturbation theory
Optimal guidance approximation synthesis via perturbation theory including linear, quadratic and higher order feedback approximation method
Space science - step rocket optimization theory
Optimal control problems for Markov chains solved by iterative method, using nonlinear finite difference equations to approximate degenerate elliptic functions
Optimal final value control theory, applying variational calculus and functional analysis to control function selection for dynamic systems
Compilation of technical papers in guidance theory, optimization theory, numerical methods, and celestial mechanics