Dynamics and autopilot design for endoatmospheric interceptors with dual control systems
Authors:
- Di ZhouDZDi Zhou
- Chuntao ShaoCSChuntao Shao
- 1 September 2009
- journal article
- Published by Elsevier in Aerospace Science and Technology
- Vol. 13 (6) , 291-300
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- Dual Aero/Propulsive Missile Control - Optimal Control and Control Allocation2006
- Missile Controlled by Lift and Divert Thrusters Using Nonlinear Dynamic Sliding ManifoldsJournal of Guidance, Control, and Dynamics, 2006
- Nonlinear dynamic autopilot design for the non-minimum phase missile2002
- Autopilot design for a missile with reaction-jet using coefficient diagram method2001
- Three-Axes Missile Autopilot Design: From Linear to Nonlinear Control StrategiesJournal of Guidance, Control, and Dynamics, 2001
- Adaptive nonlinear control of agile antiair missiles using neural networksIEEE Transactions on Control Systems Technology, 2000
- Autopilot design for highly maneuvering STT missiles via singular perturbation-like techniqueIEEE Transactions on Control Systems Technology, 1999
- Adaptive techniques for multiple actuator blending1998
- Agile Missile Dynamics and ControlJournal of Guidance, Control, and Dynamics, 1998
- A sliding mode missile pitch autopilot synthesis for high angle of attack maneuveringIEEE Transactions on Control Systems Technology, 1998