Skip to Main content Skip to Navigation
Conference papers

On-Line Optimization for Fault Tolerant Flight Control

Abstract : In this communication the case in which an aerodynamic actuator failure occurs to an aircraft while it has to perform some guidance maneuver is considered. This problem is dealt with the reassignment of remaining operational actuators in order to perform the required maneuver while maintaining the structural integrity of the aircraft. Nonlinear Inverse Control technique is used to generate online nominal moments along the three axes of the aircraft. Taking into account all material and structural constraints as well as the redundant effects from other actuators, a mathematical programming problem to be solved on-line which related to control reallocation can be formulated. Solution techniques, based on dynamic neural networks, active set methods and interior point methods are discussed and the respective performances are compared.
Document type :
Conference papers
Complete list of metadata

Cited literature [18 references]  Display  Hide  Download
Contributor : Céline Smith Connect in order to contact the contributor
Submitted on : Tuesday, January 14, 2014 - 3:30:33 PM
Last modification on : Tuesday, October 19, 2021 - 11:17:58 PM
Long-term archiving on: : Tuesday, April 15, 2014 - 4:25:46 PM


Files produced by the author(s)


  • HAL Id : hal-00930266, version 1


Lunlong Zhong, Felix Mora-Camino. On-Line Optimization for Fault Tolerant Flight Control. ISAA 2013, 3rd International Symposium on Aircraft Airworthiness, Nov 2013, Toulouse, France. ⟨hal-00930266⟩



Record views


Files downloads