Identification and optimization of aircraft dynamics.
- 1 April 1973
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 10 (4) , 193-199
- https://doi.org/10.2514/3.44364
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Design of helicopter stabilization systems using optimal control theory.Journal of Aircraft, 1969
- On an iterative technique for Riccati equation computationsIEEE Transactions on Automatic Control, 1968
- FUNDAMENTAL STUDY OF ADAPTIVE CONTROL SYSTEMSPublished by Defense Technical Information Center (DTIC) ,1962