Research on High Accuracy Guidance Law for Reentry Vehicles
Three-Dimensional Optimal Impact Time Guidance for Antiship Missiles
Cooperative Estimation and Guidance Strategy Using Bearings-Only Measurements
Generalized optimal impact-angle-control guidance with terminal acceleration response constraint
Integrated impact time guidance and control against non-maneuvering targets
Finite-time control for asteroid hovering and landing via terminal sliding-mode guidance
Sinusoidal function weighted optimal guidance laws
Robust terminal guidance law design for missiles against maneuvering targets
Angle-Constrained Terminal Guidance Using Quasi-Spectral Model Predictive Static Programming
Guidance Law Design with Fixed-Time Convergent Error Dynamics
Terminal area guidance for reusable launch vehicles
Sliding-Mode-Control–Based Instantaneously Optimal Guidance for Precision Soft Landing on Asteroid
Asteroid Precision Landing via Multiple Sliding Surfaces Guidance Techniques
Sliding mode–based simultaneous control of impact angle and impact time
Impact angle and impact velocity constrained terminal guidance for stationary target
Mars atmospheric entry guidance for optimal terminal altitude