Solution of aircraft inverse problems by local optimization
- 1 May 1995
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 18 (3) , 567-571
- https://doi.org/10.2514/3.21424
Abstract
A feedforward control technique is presented for the determination of the input/output map associated to the inverse problem of the simulated motion of an aircraft. The procedure is particularly suitable in the redundant cases, which are reduced to nominal ones by imposing physically reasonable constraints on the state variables through a focal optimization algorithm. Comparisons with already available solutions are shown together with some significant applicationsKeywords
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