Control Law and Simulation Analysis of Vertical Take-Off and Landing Stage of Tilt Rotor Aircraft

Abstract:

This paper utilized the genetic algorithm to optimize the PID controller of vertical take-off and landing stage of tilt rotor aircraft. According to the features of stability control of vertical take-off and landing stage of tilt rotor aircraft, system ascend time, steady error, and weighted overshoot are chosen as objective function of optimization. Simulation results show that PID controller designed by the genetic algorithm possess the excellent flexibility, adaptability and can produce the better control effect.

• Periodical: Advanced Materials Research (Volume 1082)
• Pages: 521-524
• DOI: https://doi.org/10.4028/www.scientific.net/AMR.1082.521
• Online since: December 2014
• Authors: Yuan Qi Zhang*, Wei Ping Zhao, Song Xiang
• Keywords: Control Law, Genetic Algorithm (GA), Landing, Tilt Rotor Aircraft, Vertical Take-Off

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