Evaluation of a second generation reconfiguration strategy for aircraft flight control systems subjected to actuator failure/surface damage
- 6 January 2003
- conference paper
- Published by Institute of Electrical and Electronics Engineers (IEEE)
Abstract
The authors report evaluation results obtained on the six-degree-of-freedom nonlinear simulation of the Grumman Combat Reconfigurable Control Aircraft (CRCA). The reconfiguration strategy consists of a robust flight control system tolerant of low-level surface damage, a hierarchical failure detection, isolation, and estimation (FDIE) system identifying actuator failures and moderate-to-serve surface damage, and a reconfiguration logic in which the pseudo surface resolver (PSR) is reconfigured after impairment to recover performance and minimize transients. Preliminary performance results are presented.<>Keywords
This publication has 3 references indexed in Scilit:
- Restructurable controls for aircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Control Logic for Parameter Insensitivity and Disturbance AttenuationJournal of Guidance, Control, and Dynamics, 1982
- Multivariable feedback design: Concepts for a classical/modern synthesisIEEE Transactions on Automatic Control, 1981