Sliding Mode Techniques Applied to the Control of a Micro Air-Vehicle
- 22 June 2003
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Multi-Input/Multi-Output Sliding Mode Control for a Tailless Fighter AircraftJournal of Guidance, Control, and Dynamics, 2003
- A control engineer's guide to sliding mode controlIEEE Transactions on Control Systems Technology, 1999
- Rotorcraft Handling Qualities in TurbulenceJournal of Guidance, Control, and Dynamics, 1995