Improvement of taxiing performance for civil airliner by active control

Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics

Volumn 29, Issue 11, 2003, Pages 1017-1021

  Jia, Yuhong ^a   Liu, Ying ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

Landing gear; Nonlinear model; Parameter identification; Self tuning control

Indexed keywords

CIVIL AVIATION; COMPUTER SIMULATION; CONTROL SYSTEMS; IDENTIFICATION (CONTROL SYSTEMS); PARAMETER ESTIMATION;

CIVIL AIRLINER; NONLINEAR MODEL; PARAMETER IDENTIFICATION; TAXIING PERFORMANCE;

LANDING GEAR (AIRCRAFT);

EID: 1542712601     PISSN: 10015965     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (5)

1. Jia Yuhong, He Qingzhi, Yang Guozhu. Taxing performance analysis of active control of landing gear[J]. Acta Aeronautica et Astronautica Sinica, 1999, 20(6): 545-548 (in Chinese)
2. Li Qingquan. Theory, design and applications of adaptive control[M]. Beijing: Science Press, 1990. 249-310 (in Chinese)
3. John R M, Huey D C. A mathematical model of an active control landing gear for load control during impact and roll-out[R]. NASA TND8080, 1976
4. Wu Shichang, Zang Yingzhi. Adaptive control[M]. Beijing: China Machine Press, 1989. 135-173 (in Chinese)
5. Wu Guangyu. System identification and adaptive control[M]. Harbin: The Press in Harbin Institute of Technology, 1987. 48-242 (in Chinese)