Proportional Navigation With Adaptive Terminal Guidance For Aircraft Rendezvous (Preprint)
AIR FORCE RESEARCH LAB WRIGHT-PATTERSON AFB OH AIR VEHICLES DIRECTORATE
Pagination or Media Count:
1. PN with adaptive terminal guidance is shown to be a viable guidance method for aircraft rendezvous in 6DOF simulation. 2. Adaptive PN and Velocity controller combination is shown to effect successful rendezvous. 3. Adaptation accounts for errors caused by assumptions stationary RZ location, wind, and tanker maneuvers.
- Military Aircraft Operations
- Navigation and Guidance