Finite element method for optimal guidance of an advanced launch vehicle
- 1 May 1992
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 15 (3) , 664-671
- https://doi.org/10.2514/3.20889
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Weak Hamiltonian finite element method for optimal control problemsJournal of Guidance, Control, and Dynamics, 1991
- New necessary conditions of optimality for control problems with state-variable inequality constraintsJournal of Mathematical Analysis and Applications, 1971