Add to ORKGDynamic programming and multistage decision processes in guidance, flight mechanics, and trajectory optimizatio
Computer program constructs a sequence of optimal solutions to dynamically-approximate linear equati...
While continuing the application of the inverse dynamics approach in obtaining the optimal numerical...
Documentation of the NBODY trajectory optimization program is presented in the form of a mathematica...
Three numerical procedures for Mayer classical and non-classical problems in trajectory optimizatio
Guidance, flight mechanics, and trajectory optimization - calculus of variations and modern applicat...
Entry guidance equations, reference trajectories, and guidance system mechanizatio
Mathematical formulation of guidance equations and solutions for orbital space mission
Maxima-minima theory, Pontryagin principle, and calculus of variations for optimal trajectory and co...
Variational calculus, gradient methods, maximum principle, and dynamic programing methods of optimal...
General perturbations theory applications to spacecraft guidance, flight mechanics, and trajectory o...
Mission constraints and trajectory interfaces for launch, rendezvous, spatial, deorbit, and entry ph...
Dynamic programming applied to guidance correction for perturbed trajectory of spacecraf
Observation theory and sensors applicable to navigation of boost and space vehicle
Computer program for trajectory optimization and payload maximization in multistage launch vehicle
Analytical approaches to path-adaptive guidance functions, circular orbit trajectories, and use of F...
Computer program constructs a sequence of optimal solutions to dynamically-approximate linear equati...
While continuing the application of the inverse dynamics approach in obtaining the optimal numerical...
Documentation of the NBODY trajectory optimization program is presented in the form of a mathematica...
Three numerical procedures for Mayer classical and non-classical problems in trajectory optimizatio
Guidance, flight mechanics, and trajectory optimization - calculus of variations and modern applicat...
Entry guidance equations, reference trajectories, and guidance system mechanizatio
Mathematical formulation of guidance equations and solutions for orbital space mission
Maxima-minima theory, Pontryagin principle, and calculus of variations for optimal trajectory and co...
Variational calculus, gradient methods, maximum principle, and dynamic programing methods of optimal...
General perturbations theory applications to spacecraft guidance, flight mechanics, and trajectory o...
Mission constraints and trajectory interfaces for launch, rendezvous, spatial, deorbit, and entry ph...
Dynamic programming applied to guidance correction for perturbed trajectory of spacecraf
Observation theory and sensors applicable to navigation of boost and space vehicle
Computer program for trajectory optimization and payload maximization in multistage launch vehicle
Analytical approaches to path-adaptive guidance functions, circular orbit trajectories, and use of F...
Computer program constructs a sequence of optimal solutions to dynamically-approximate linear equati...
While continuing the application of the inverse dynamics approach in obtaining the optimal numerical...
Documentation of the NBODY trajectory optimization program is presented in the form of a mathematica...