Optimal City-Center Takeoff Operation of Tiltrotor Aircraft in One Engine Failure
Publication: Journal of Aerospace Engineering
Volume 17, Issue 1
Abstract
This paper investigates optimal tiltrotor flight trajectories and performance in vertical takeoff operations from a city-center heliport considering the possibility of one engine failure. A two-dimensional longitudinal rigid body model of a tiltrotor aircraft is used. Tiltrotor flights after engine failure in both continued takeoff and rejected takeoff are formulated as nonlinear optimal control problems that minimize the heliport size, subject to various constraints from safety considerations and tiltrotor performance limitations. These problems are parametrized via collocation into parameter optimization for numerical solutions. Extensive numerical solutions are obtained, and sensitivity analyses are conducted to examine effects of model parameter uncertainties. Optimization results indicate that the maximum gross weight capability of a tiltrotor in a vertical operation is determined by the need for safe landing in the event of a single engine failure. The height at which the decision for either continuing or rejecting the takeoff is made depends on the need to maintain sufficient height during the continued takeoff flight after an engine failure.
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Information
Published In
Journal of Aerospace Engineering
Volume 17 • Issue 1 • January 2004
Pages: 26 - 39
Copyright
Copyright © 2004 American Society of Civil Engineers.
History
Received: Apr 1, 2003
Accepted: Jul 31, 2003
Published online: Dec 15, 2003
Published in print: Jan 2004
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