Flight Control Law Design via Pole Placement

Zheng Zai Qian; Xiao Hua Zhai

doi:10.4028/www.scientific.net/AMR.466-467.1202

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 466-467Flight Control Law Design via Pole Placement

Flight Control Law Design via Pole Placement

Abstract:

Modern aircraft is designed generally with static unstable configuration in order to achieve the good maneuvering performance and the good controllability. Flight control law design is very important for the modern aircraft. The most importance for the flight control law is sustained flight. This paper presents a method of the state space description static instability mathematic model of modern aircraft. A new flight control law design based on pole placement and state feedback method is given in this paper also. The flight system stability and maneuverability are greatly improved through the method of the pole placement and state feedback. The simulation results show that pole placement method is very important and feasible in modern flight control system design.

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Periodical:

Advanced Materials Research (Volumes 466-467)

Pages:

1202-1206

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.466-467.1202

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Online since:

February 2012

Authors:

Zheng Zai Qian, Xiao Hua Zhai

Keywords:

Flight Control Law, Pole Placement, Simulation, State Feedback

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References

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