Stability and Robustness Analysis of Dynamic Inversion Control Laws for Nonlinear Control of Fighter Aircraft
Aircraft dynamics are well modeled by a standard system of nonlinear ODEs (cf.  and ). Experience in industry shows that pilot simulations based on these nonlinear finite-dimensional models are very good.
Partition the flight envelope into several separate operating regimes (flight conditions).
In each regime, the aircraft dynamics are approximately represented by a linear model.
KeywordsAssure Peri Stein Librium Hines
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