Research on Technology of Thrust Asymmetry Lateral Compensation for Large Aircraft

Article Preview

Abstract:

Thrust asymmetry is dangerous for aircraft, especially in the phases of approach and landing. This paper proposes a new technology to compensate the thrust asymmetry in lateral of large aircraft. The dynamic characteristics of aircraft with asymmetric thrust are firstly analyzed in the paper. Then, the controllability conditions and balanced flight attitude in the case of thrust asymmetry are studied. Based on the mathematic model of Airbus 300, a thrust asymmetry lateral compensator is designed for the phases of approach and landing to ensure the safety of approach and landing. Numerical simulation results show that the designed compensator (control law) can compensate the asymmetric thrust very well.

You might also be interested in these eBooks

Info:

Periodical:

Advanced Materials Research (Volumes 383-390)

Pages:

1256-1261

Citation:

Online since:

November 2011

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2012 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Han Fengbo, Yu Xinjiang, and Fang Dan, Discussion on non-symmetric thrust flight for a certain type of the large transporter, Flight Dynamics, vol. 15, pp.80-83, Sep (1997).

Google Scholar

[2] Jim, McWha, Development of the 777 flight control system, 2003 AIAA Guidance, Navigation, and Control Conference and Exhibit, Austin, TX, Aug (2003).

DOI: 10.2514/6.2003-5767

Google Scholar

[3] Kelly Latimer, James Ross, C-17 Engine-Out Compensation System Testing, 1999 IEEE Aerospace Conference, vol. 3, pp.43-51, (1999).

DOI: 10.1109/aero.1999.789763

Google Scholar

[4] FAR Part25.

Google Scholar

[5] Horlings, Harry, Staying alive with a dead engine, 18th Annual European Aviation Safety Seminar, (2006).

Google Scholar

[6] Rudolf Brockhaus, Flugregelung, pp.568-576, (1999).

Google Scholar