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International Conference on Mechanical and Electrical Technology, 3rd, (ICMET-China 2011), Volumes 1–3

By
Yi Xie
Yi Xie
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ISBN:
9780791859810
No. of Pages:
906
Publisher:
ASME Press
Publication date:
2011

In this paper, we address the problem of identification and control of a small-scaled unmanned helicopter system, which consisted of flight control system (FCS) and ground control system (GCS). In order to perform automatic flight, we did system identification experiments to model the dynamic characteristics of the helicopter. Low-order models of roll, pitch and yaw channel are identified. The identified models are proved can provide a good match of helicopter dynamic characteristics for flight control research.

Abstract
Key Words
1 Introduction
2. Vehicle Description
3 Flight Control System
4. System Identification Expriments
5. Summaries
References
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