Design and piloted simulator evaluation of adaptive safe flight envelope protection algorithm

Design and piloted simulator evaluation of adaptive safe flight envelope protection algorithm

Design and evaluation of a Flight Envelope Protection haptic feedback system

This paper describes the design and evaluation of a shared control, haptic feedback system to communicate Flight Envelope Protection System intent. The concept uses a combination of stiffness feedback and vibration to communicate proximity of the aircraft state to flight envelope boundaries. In addition, a stick center shift can be applied by...

Model-based fault detection and identification with online aerodynamic model structure selection

This publication describes a recursive algorithm for the approximation of time-varying nonlinear aerodynamic models by means of a joint adaptive selection of the model structure and parameter estimation. This procedure is called adaptive recursive orthogonal least squares (AROLS) and is an extension and modification of the previously developed...

A benchmark for fault tolerant flight control evaluation

A large transport aircraft simulation benchmark (REconfigurable COntrol for Vehicle Emergency Return ? RECOVER) has been developed within the GARTEUR (Group for Aeronautical Research and Technology in Europe) Flight Mechanics Action Group 16 (FM-AG(16)) on Fault Tolerant Control (2004 2008) for the integrated evaluation of fault detection and...