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Proceedings Paper

Piecewise linear control allocation for flying wing UAV
Author(s): Peng Wang; Zhou Zhou
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Paper Abstract

A piecewise linear control allocation approach was presented for the solution of the non-linear control allocation problem for flying wing Unmanned Aerial Vehicle (UAV). The presented approach utilizes the piecewise linear assumption for the control effector moment data. This assumption allows the non-linear control allocation problem to be cast as a piecewise linear program. In order to solve the piecewise linear program, it was re-formulated as a mixed-integer linear program. The discussed mixed-integer linear programs were implemented in a nonlinear Simulink simulation of a flying wing UAV landing phase. The analysis of the simulation results showed that the piecewise linear program approach results in improved tracking performance when compared to a more traditional control allocation approach that uses a linear approximation of the control moments, especially when the aircraft is subjected to control effector failures.

Paper Details

Date Published: 10 November 2007
PDF: 7 pages
Proc. SPIE 6795, Second International Conference on Space Information Technology, 67950Y (10 November 2007); doi: 10.1117/12.773337
Show Author Affiliations
Peng Wang, Northwestern Polytechnical Univ. (China)
Zhou Zhou, Northwestern Polytechnical Univ. (China)


Published in SPIE Proceedings Vol. 6795:
Second International Conference on Space Information Technology

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