High-Performance Attitude Control Design of Supersonic Tailless Aircraft: A Cascaded Disturbance Rejection Approach

This paper focuses on the triaxial augmentation ability of active disturbance rejection control (ADRC) technique tailless layout with a fully moving wing tip to achieve high performance for supersonic aircraft. Firstly, stability characteristics and controllability flying are analyzed determine coupling this kind Secondly, an attitude controller is designed based ADRC theory, linear frequency domain analysis method introduced analyze influence bandwidth extended stator system. In addition, tuning process law given. Carrier dropping simulations flight missions under nominal condition, model parameter perturbation, wind conducted. The results show that can full-speed wing. work has potential significantly boost engineering acceptability robustness aircraft design in real-world scenarios. presented cascaded approach improve vehicles.