Time-Domain Finite Element Method for Inverse Problem of Aircraft Maneuvers
- 1 January 1997
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 20 (1) , 97-103
- https://doi.org/10.2514/2.4000
Abstract
No abstract availableKeywords
This publication has 12 references indexed in Scilit:
- Finite element method for the solution of state-constrained optimal control problemsJournal of Guidance, Control, and Dynamics, 1995
- Solution of aircraft inverse problems by local optimizationJournal of Guidance, Control, and Dynamics, 1995
- Optimal aircraft terrain-following analysis and trajectory generationJournal of Guidance, Control, and Dynamics, 1995
- Inverse simulation of large-amplitude aircraft maneuversJournal of Guidance, Control, and Dynamics, 1993
- Inverse dynamics approach to trajectory optimization for an aerospace planeJournal of Guidance, Control, and Dynamics, 1993
- Errata: Finite Element Method for Optimal Guidance of an Advanced Launch VehicleJournal of Guidance, Control, and Dynamics, 1992
- Inverse and optimal control for desired outputsJournal 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
- An interpretation of airplane general motion and contol as inverse problemJournal of Guidance, Control, and Dynamics, 1986