Propulsion control of crippled aircraft by H(infinity) model matching

n ;For the longitudinal motion, an algorithm is developed to synthesize an controller such that the response of the crippled airplane matches the response of the nominal model. Simulations on three different airplane models demonstrate the concept. For the lateral motion, an ;Next, a neural network approach to gain scheduling linear dynamic controllers for PCA system is presented. To generate the training set, linear controllers are synthesized by the...