Research and Application of Fault Diagnosis Method Based on Time Fault Propagation Graph
Influence of Continuous Jet at the Lower Surface on Airfoil Aerodynamic Performance
Design of Aircraft Attitude Control Law Based on Constrained Incremental Backstepping
Robust Flight Controller Design Based on Adaptive Nonlinear Dynamic Inverse with Reference Model
Adaptive Guidance Law of Laser-Guided Bomb Based on Sliding Mode Variable Structure
An Incremental Nonlinear Dynamic Inversion with Prescribed Performance for Damaged Aircraft