- Studied RL agent based Guidance Laws and Optimal Control techniques for Surface-to-Air Missile Guidance
- Simulated optimal trajectory for surface to air ballistic missile by implementing Gradient method as optimization technique in MATLAB under the guidance of Dr. Prem Kumar(Scientist- ‘F’, DOS)}
- Implemented Proportional Navigation(PN Classical Guidance law) on a point mass 3-d model in MATLAB with lofting and used it as a baseline for performance evaluation against RL agent based guidance laws
-
Notifications
You must be signed in to change notification settings - Fork 5
Studied RL agent-based Guidance Laws and Optimal Control techniques for Surface-to-Air Missile Guidance. Simulated optimal trajectory for the surface to air ballistic missile by implementing Gradient method as optimization technique in MATLAB
License
sankalp-s/Missile-Guidance-and-RL
Folders and files
| Name | Name | Last commit message | Last commit date | |
|---|---|---|---|---|
Repository files navigation
About
Studied RL agent-based Guidance Laws and Optimal Control techniques for Surface-to-Air Missile Guidance. Simulated optimal trajectory for the surface to air ballistic missile by implementing Gradient method as optimization technique in MATLAB
Resources
License
Stars
Watchers
Forks
Releases
No releases published
Packages 0
No packages published