Modeling and Simulation of the Helicopter Control System Based on the Flight Qualities

Cheng Wen Jian; Shu Li; Ji Zhang

doi:10.4028/www.scientific.net/AMR.1030-1032.1493

Paper Titles

Development and Trend of Intelligent Monitoring System for Greenhouse
p.1475

Embedded Systems Based on Simple GPS Auto Navigation System
p.1480

Study on Online Monitoring System of Power Transformer
p.1484

Intelligent Self-Adaptive Control Method Based on RBFNN and its Application in Hydraulic Control
p.1488

Modeling and Simulation of the Helicopter Control System Based on the Flight Qualities
p.1493

Online Monitoring and Alarm System of the Galvanized Steel Wire’s Weight Based on OPC
p.1498

OPC Automation System Interconnection Interface
p.1502

Research of Application Status for the Drive Motor Based on the Pure Electric Vehicle
p.1505

Research of Greenhouse Environment Monitoring System
p.1509

HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 1030-1032Modeling and Simulation of the Helicopter Control...

Modeling and Simulation of the Helicopter Control System Based on the Flight Qualities

Abstract:

Helicopter is a strong coupling and instability nonlinear system, of which the inherent flight qualities are poor. Helicopter model following control technology can make four control channels of helicopter with excellent tracking and decoupling characteristics. This paper applied the control method of model following control combining eigenststructure assignment to the helicopter control system. The results of simulation show that the helicopter flight qualities meet the requirements of ADS-33, the helicopter has excellent tracking and decoupling characteristics. Thus it proves that this control method is of great effectiveness.

You might also be interested in these eBooks

Materials, Transportation and Environmental Engineering II

View Preview

Info:

Periodical:

Advanced Materials Research (Volumes 1030-1032)

Pages:

1493-1497

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.1030-1032.1493

Citation:

Cite this paper

Online since:

September 2014

Authors:

Cheng Wen Jian*, Shu Li, Ji Zhang

Keywords:

Eigenststructure Assignment, Flight Control, Flight Qualities, Helicopter, Model Following Control

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

* - Corresponding Author

References

[1] Heinz Erzberger. Analysis and Design of Model Following Control Systems by State Space Techniques. Scientific and Technical Report, 68A36541, United States: NASA, (1968).

Google Scholar

[2] Rong Xiaolu. The Design Methods Research of Helicopter Flight Quality. Nan Jing: Nanjing University of Aeronautics and Astronautics, (2007).

Google Scholar

[3] Handling Qualities Requirements for Military rotorcraft, Aeronautical Design Standard, ADS-33D, United States Army Aviation and Troop Command, July, (1994).

Google Scholar