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CEAS EuroGNC 2019

Flight Envelope Protections Using Phase Plane Limits and Backstepping Control

Rasmus Steffensen Technical University of Munich
Agnes Gabrys Technical University of Munich
Florian Holzapfel Technical University of Munich
Abstract:
This paper introduces a new way to enforce aircraft flight envelope protections based on specifications in the phase plane of a protected variable. The protection is based on applying backstepping on a set of transformed coordinates, such that accurate phase plane tracking can be achieved. Piecewise polynomials are proposed for the limit in the phase plane, to obtain less conservative protections that enhance the aircraft performance around the protected variables. The approach has a well defined and intuitive response behaviour close to the limit in which the distance from the limit is defined with a constant time to violation. Above the limit, aggressive disturbance rejection can be achieved. The results are shown in simulation of a multi engine general aviation aircraft.
Keywords: Aircraft flight control analysis and design; Tracking
CEAS-GNC-2019-003PDF is not available online. Authors may distribute copies of their paper or contact the CEAS GNC TC chair to make their paper available through the EuroGNC paper archive.


Rasmus Steffensen, Agnes Gabrys, Florian Holzapfel: Flight Envelope Protections Using Phase Plane Limits and Backstepping Control. Proceedings of the 2019 CEAS EuroGNC conference. Milan, Italy. April 2019. CEAS-GNC-2019-003.
BibTeX entry:

@Incollection{CEAS-GNC-2019-003,
    authors = {Steffensen, Rasmus and Gabrys, Agnes and Holzapfel, Florian},
    title = {Flight Envelope Protections Using Phase Plane Limits and Backstepping Control},
    booktitle = {Proceedings of the 2019 {CEAS EuroGNC} conference},
    address = {Milan, Italy},
    month = apr,
    year = {2019},
    note = {CEAS-GNC-2019-003}
}