A three-dimensional terminal guidance law that meets the constraints is designed for the terminal attack of unpowered gliding vehicle on the ground static target. Considering that the dynamic pressure and impact angle constraints should be considered simultaneously in this process, a new time-varying terminal impact angle function method is proposed, thus determining the terminal guidance law. Through the simulation of CAV-L, the feasibility of the method and terminal strike accuracy are verified.
A Three-Dimensional Terminal Guidance Law for Unpowered Gliding Vehicles Considering Dynamic Pressure and Impact Angle Constraints
Lect. Notes Electrical Eng.
2021-10-30
13 pages
Article/Chapter (Book)
Electronic Resource
English
British Library Conference Proceedings | 2022
|Impact speed and angle constrained guidance law for unpowered gliding vehicle
Elsevier | 2025
|An Approximate Optimal Maximum Range Guidance Scheme for Subsonic Unpowered Gliding Vehicles
DOAJ | 2015
|