Robust autopilot design for future missile systems
- 11 August 1997
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 19 references indexed in Scilit:
- Design of robust, time-varying controllers for missile autopilotsPublished by Institute of Electrical and Electronics Engineers (IEEE) ,2003
- Application of H/sup /spl infin// control to pitch autopilot of missilesIEEE Transactions on Aerospace and Electronic Systems, 1996
- High-Performance, Robust, Bank-to-Turn Missile Autopilot DesignJournal of Guidance, Control, and Dynamics, 1995
- Gain scheduling for H-infinity controllers: a flight control exampleIEEE Transactions on Control Systems Technology, 1993
- The complex structured singular valueAutomatica, 1993
- Beyond singular values and loop shapesJournal of Guidance, Control, and Dynamics, 1991
- Robust autopilot design using μ-synthesisPublished by Institute of Electrical and Electronics Engineers (IEEE) ,1990
- Missile autopilot design using H∞ optimal control with μ-synthesisPublished by Institute of Electrical and Electronics Engineers (IEEE) ,1990
- Applying mu -synthesis to missile autopilot designPublished by Institute of Electrical and Electronics Engineers (IEEE) ,1990
- Robust instrumentation configurations for homing missile flight controlPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980