JACIII Vol.22 No.3 pp. 316-322
doi: 10.20965/jaciii.2018.p0316


Gain-Scheduled for Aerial Vehicle Autopilot Design Using Fixed-Structure Synthesis

Bin Li*,†, Defu Lin*, Song Tian*, and Zhe Yang**

*School of Aerospace Engineering, Beijing Institute of Technology
No. 5, Zhong Guan Cun South Street, Haidian District, Beijing 100081, China

**International Armament Research & Development Center
12A Guang An Men Nan Jie, Beijing 100053, China

Corresponding author

November 9, 2017
March 5, 2018
May 20, 2018
gain-scheduled, fixed-structure synthesis, aerial vehicle autopilot, hidden coupling terms, gain surface tuning

A novel systematic technique for gain-scheduled control based on fixed-structure synthesis is adopted to design the aerial vehicle autopilot. The gain-scheduled design can be transformed into the multi-model control problem with both controller architecture and gain-scheduled architecture defined a priori. Hidden coupling terms naturally arise in the linearized dynamics of the gain-scheduled controller when some of the state variables are also used as scheduling variables. Unlike traditional approaches that do not consider these terms, the proposed method takes the hidden coupling terms directly into account in the synthesis phase. Finally, numerical simulations are carried out to evaluate the effectiveness of the proposed methods.

Threeloop autopilot architecture

Threeloop autopilot architecture

Cite this article as:
B. Li, D. Lin, S. Tian, and Z. Yang, “Gain-Scheduled for Aerial Vehicle Autopilot Design Using Fixed-Structure Synthesis,” J. Adv. Comput. Intell. Intell. Inform., Vol.22 No.3, pp. 316-322, 2018.
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Last updated on Jul. 23, 2024