摘要: A manual flight control system for the lateral directional dynamics of a modernfighter aircraft incorporating thrust vectoring is presented. Design goals are posed in terms of maintaining acceptable flying qualities during high al... 展开 A manual flight control system for the lateral directional dynamics of a modernfighter aircraft incorporating thrust vectoring is presented. Design goals are posed in terms of maintaining acceptable flying qualities during high alpha maneuvering while also achieving robustness to model parameter variations and unmodeled dynamics over the entire flight envelope. The need for gain scheduling is eliminated by using an inner loop dynamic inversion/outer loop structured 收起