The solution of a launch vehicle trajectory problem by an adaptive finite-element method

Author:

Estep Donald J.,Hodges Dewey H.,Warner Michael

Publisher

Elsevier BV

Subject

Computer Science Applications,General Physics and Astronomy,Mechanical Engineering,Mechanics of Materials,Computational Mechanics

Reference23 articles.

1. R.H. Battin, An Introduction to the Mathematics and Methods of Astrodynamics, AIAA, Washington, DC, 1987

2. R. Bless, Time-domain finite elements in optimal control with application to launch vehicle guidance, Ph.D. thesis, School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, GA 30332, 1991

3. Finite element solution of optimal control problems with stat-control inequality constraints;Bless;J. Guid. Control Dynam.,1992

4. Finite element method for the solution of state-constrained optimal control problems;Bless;J. Guid. Control Dynam.,1995

5. Earth aerobraking strategies for manned return from mars;Braun;J. Spacecraft Rockets,1992

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1. A full-space quasi-Lagrange-Newton-Krylov algorithm for trajectory optimization problems;ETNA - Electronic Transactions on Numerical Analysis;2018

2. Parametric variational solution of linear-quadratic optimal control problems with control inequality constraints;Applied Mathematics and Mechanics;2014-07-17

3. Optimization in simulations of human movement planning;International Journal for Numerical Methods in Engineering;2011-02-21

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