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 .
Azab, A. (1985). ADAPTIVE CONTROL OF LONGITUDINAL FLIGHT OF AIRCRAFT SYSTEM. International Conference on Aerospace Sciences and Aviation Technology, 1(A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO), 873-895. doi: 10.21608/asat.1985.26564
MLA
A. A. Azab. "ADAPTIVE CONTROL OF LONGITUDINAL FLIGHT OF AIRCRAFT SYSTEM". International Conference on Aerospace Sciences and Aviation Technology, 1, A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO, 1985, 873-895. doi: 10.21608/asat.1985.26564
HARVARD
Azab, A. (1985). 'ADAPTIVE CONTROL OF LONGITUDINAL FLIGHT OF AIRCRAFT SYSTEM', International Conference on Aerospace Sciences and Aviation Technology, 1(A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO), pp. 873-895. doi: 10.21608/asat.1985.26564
VANCOUVER
Azab, A. ADAPTIVE CONTROL OF LONGITUDINAL FLIGHT OF AIRCRAFT SYSTEM. International Conference on Aerospace Sciences and Aviation Technology, 1985; 1(A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO): 873-895. doi: 10.21608/asat.1985.26564
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