Adaptive control laws for F-8 flight test
- 1 October 1977
- journal article
- Published by Institute of Electrical and Electronics Engineers (IEEE) in IEEE Transactions on Automatic Control
- Vol. 22 (5) , 758-767
- https://doi.org/10.1109/tac.1977.1101605
Abstract
No abstract availableThis publication has 14 references indexed in Scilit:
- The stochastic control of the F-8C aircraft using the multiple model adaptive control (MMAC) methodPublished by Institute of Electrical and Electronics Engineers (IEEE) ,1975
- Application of likelihood ratio methods to failure detection and identification in the NASA F-8 DFBW aircraftPublished by Institute of Electrical and Electronics Engineers (IEEE) ,1975
- An implementable digital adaptive flight controller designed using stabilized single stage algorithmsPublished by Institute of Electrical and Electronics Engineers (IEEE) ,1975
- Adaptive control using a moving window Newton-Raphson parameter identification schemePublished by Institute of Electrical and Electronics Engineers (IEEE) ,1975
- Management of analytical redundancy in digital flight control systems for aircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Optimal inputs for linear system identificationIEEE Transactions on Automatic Control, 1974
- Design and flight experience with a digital fly-by-wire control system using Apollo guidance system hardware on an F-8 aircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- The role and use of the stochastic linear-quadratic-Gaussian problem in control system designIEEE Transactions on Automatic Control, 1971
- Application of optimal control to perfect model followingJournal of Aircraft, 1970
- A parameter-adaptive control techniqueAutomatica, 1969