Quasi-optimum design of an aircraft landing control system
- 1 January 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 7 (1) , 38-43
- https://doi.org/10.2514/3.44119
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Synthesis of feedback controls using optimization theory--An exampleIEEE Transactions on Automatic Control, 1963