Analytical research in guidance theory Final technical report, 15 Sep. 1966 - 31 Oct. 1967
Applying calculus of variations to optimal guidance problems, and symbolic programming of polynomials
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Applying calculus of variations to optimal guidance problems, and symbolic programming of polynomials
Bolza problem of calculus of variations in terms of control coding applied to trajectories
Variational calculus used in obtaining lift drag ratio attainable by slender conical body at hypersonic speeds
Relation between optimal control problem and Liapunov functions, and calculus of variations and maximum principle methods of solving synthesis problems
Guidance regime for optimal multistage lunar trajectory derived by applying calculus of variations to generalized Bolza problem
Multiple solutions to problem of bolza in calculus of variation
Calculus of variations minimized under linearized differential constraint for hybrid gradient method
Minimum drag bodies in hypersonic flow using calculus of variations
Book on space clinical medicine covering hypoxia, ebullism, decompression, aerotitis, dehydration, hypothermia, cabin atmosphere contamination, urinary calculus, etc
Low thrust trajectories for minimum time rendezvous between continuous thrust interceptor and passive target vehicle, comparing calculus of variations and steepest ascent analyses
Bolza problem of calculus of variations extended to trajectory optimization problems with several subarcs
Transforming optical control problem into equivalent Lagrange problem in calculus of variations
Second order endpoint condition considered in solution of Bolza problem in calculus of variations
Five dimensional rotations and representation of isomorphic spinor groups by boson operators calculus, expanding Gelfand states in Weyl patterns
Analytical approach to gradient method within framework of Bolza problem of variational calculus, using linearized differential and isoperimetric constraints
Calculus of variations used for determining optimum one dimensional MHD slider bearing with bounded control variables
Endpoint sufficiency test based on differential calculus method, considering Bolza problem of continuous state and piecewise control variables
Optimal control surface location for flexible aircraft determined by matrix minimum principle and calculus of variations