Acceleration, gamma, and theta guidance for abort landing in a windshear
- 1 November 1989
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 12 (6) , 815-821
- https://doi.org/10.2514/3.20486
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Penetration landing guidance trajectories in the presence of windshearJournal of Guidance, Control, and Dynamics, 1989
- Gamma guidance schemes for flight in a windshearJournal of Guidance, Control, and Dynamics, 1988
- Optimization and acceleration guidance of flight trajectories in a windshearJournal of Guidance, Control, and Dynamics, 1987
- Primal-dual properties of sequential gradient-restoration algorithms for optimal control problems 2. General problemJournal of Mathematical Analysis and Applications, 1986