Dual Aero/Propulsive Missile Control - Optimal Control and Control Allocation
Authors:
- 15 June 2006
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Optimal Control Solution for Dual (Tail and Canard) Controlled Missiles2006
- A Miss Distance Study for Homing Missiles: Tail vs Canard Control2006
- Missile Longitudinal Autopilots: Connections Between Optimal Control and Classical Topologies2005
- Missile Longitudinal Autopilots: Comparison of Multiple Three Loop Topologies2005
- Resolving actuator redundancy—optimal control vs. control allocationAutomatica, 2005