Control variables for finite element solution of missile trajectory optimization
- 1 September 1995
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 18 (5) , 1208-1211
- https://doi.org/10.2514/3.21528
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Finite element solution of optimal control problems with state-control inequality constraintsJournal of Guidance, Control, and Dynamics, 1992
- Finite element method for optimal guidance of an advanced launch vehicleJournal of Guidance, Control, and Dynamics, 1992
- Weak Hamiltonian finite element method for optimal control problemsJournal of Guidance, Control, and Dynamics, 1991