An optimal guidance approximation theory
Optimal guidance approximations using perturbation theory
OPTIMAL CONTROL↗
Engineering topics
Publications and source records attributed to Kelley, H. J..
Optimal guidance approximations using perturbation theory
Optimization of trajectory achieved by successive approximation method based on second variation theory
Derivation of the singular extremals of lawdens problem of optimal rocket flight by use of the legendre-clebsch necessary condition applied in a transformed system of state and control variables
Optimal rocket flight in gravitation field
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