Reconfigurable flight control using nonlinear dynamic inversion with a special accelerometer implementation

This publication has 2 references indexed in Scilit:

• Indirect adaptive flight control system interactions
  International Journal of Robust and Nonlinear Control, 1999
• Implementation and flight test assessment of an adaptive, reconfigurable flight control system
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1997