Adaptive Guidance Law of Laser-Guided Bomb Based on Sliding Mode Variable Structure
Design of Aircraft Attitude Control Law Based on Constrained Incremental Backstepping
Influence of Continuous Jet at the Lower Surface on Airfoil Aerodynamic Performance
Research and Application of Fault Diagnosis Method Based on Time Fault Propagation Graph
Research on Distributed Target Allocation in Multi-UAV Beyond Visual Range Cooperative Air Combat
Robust Flight Controller Design Based on Adaptive Nonlinear Dynamic Inverse with Reference Model