ADAPTIVE CONTROL OF LONGITUDINAL FLIGHT OF AIRCRAFT SYSTEM | ||||
| International Conference on Aerospace Sciences and Aviation Technology | ||||
| Article 73, Volume 1, A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO, May 1985, Page 873-895 PDF (3.74 MB) | ||||
| Document Type: Original Article | ||||
| DOI: 10.21608/asat.1985.26564 | ||||
 View on SCiNiTO | ||||
| Author | ||||
| A. A. Azab | ||||
| Visiting professor at Aero. Eng. Dept. Iowa State University, Ames, Iowa, 50011 . Originally With Military Technical College, Cairo, Egypt . | ||||
| Abstract | ||||
| This Paper present two proposals for adaptive control of supersonic aircraft. Inthe first proposal, the aircraft complete transfer function is controlled to behave according to a second order chosen model, while in the second proposal the inner loop of the aircraft transfer function is controlled to behave according to a first order model. A modified gradient technique for a model reference adaptive control system with less order model is employed in the two proposals. Analog computer simulation resuits are presented and discussed . | ||||
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