A fault-tolerant approach to helicopter swashplate control
- 1 January 1985
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 8 (1), 62-70
- https://doi.org/10.2514/3.19936
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Applied Optimal ControlPublished by Taylor & Francis ,2018
- Generalized Likelihood Test for FDI in Redundant Sensor ConfigurationsJournal of Guidance and Control, 1979