Title
Gain scheduled missile autopilot design using observer-based H∞ control
Document Type
Conference Proceeding
Publication Date
1-1-1995
Abstract
This paper studies gain scheduled autopilot design in the pitch axis. To achieve the tracking specification with both stability and performance robustness for pitch autopilot design, frequency shaping is adopted and H∞ optimization is employed. It is shown that with suitable modification of the design objective in [11], the resulting central H∞ controller has an observer form and it can be computed without iteration. This is especially attractive for gain schedule implementation. The performance of a typical pitch autopilot synthesized by the proposed design method is then evaluated by computer simulations.
Publication Source (Journal or Book title)
Proceedings of the American Control Conference
First Page
1951
Last Page
1955
Recommended Citation
Gu, G., Cloutier, J., & Kim, G. (1995). Gain scheduled missile autopilot design using observer-based H∞ control. Proceedings of the American Control Conference, 3, 1951-1955. Retrieved from https://repository.lsu.edu/eecs_pubs/372