An algorithm is presented for the identi"cation of aircraft stability derivatives and distributed control derivatives, in real time. Feedback control correlates the e!ectors' displacement with the aerodynamic angles, while the most commonly used control allocation algorithms correlate the e!ectors.
β¦ LIBER β¦
On One Identification Problem for Distributed Controllable Systems
β Scribed by Shklyar, Benzion; Bakhmutsky, Victor
- Book ID
- 118209230
- Publisher
- Society for Industrial and Applied Mathematics
- Year
- 1994
- Tongue
- English
- Weight
- 907 KB
- Volume
- 32
- Category
- Article
- ISSN
- 0363-0129
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