Citation: | L&, Shaojie, Cao Yihua, Li Guozhi, . Influences of aerodynamic configuration parameters on helicopter flying qualities[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(1): 54-58. (in Chinese) |
[1] |
Celi R.Design sensitivity analysis and optimization for helicopter handling qualities improvement[D].Maryland:Univ of Maryland, 2002
|
[2] |
Fusato D, Celi R.Design sensitivity analysis for helicopter flight dynamic and aeromechanic stability[J].Journal of Guidance, Control, and Dynamics, 2003, 26(6):918-923
|
[3] |
Kumar M V, Sampath P, Suresh S, et al.Design of a stability augmentation system for a helicopter using LQR control and ADS-33 handling qualities specifications[J].Aircraft Engineering and Aerospace Technology, 2008, 80(2):111-123
|
[4] |
Cao Yihua, Li Guozhi, Yang Qian.Studies of trims, stability, controllability, and some flying qualities of a tandem rotor helicopter[J].Journal of Aerospace Engineering, 2009, 223(G2): 171-177
|
[5] |
Hilbert K B.A mathematical model of UH-60 helicopter[R].NASATM85890, 1984
|
[6] |
Padfield G D.Helicopter flight dynamics[M].New York:Wiley-Blackwell, 2007
|
[7] |
BallinM G.Validation of a real-time engineering simulation of the UH-60A helicopter[R].NASA TM88359, 1987
|
[8] |
Howlett J J.UH-60A black hawk engineering simulation program:volume I-mathematical model[R].NASA CR166309, 1981
|
[9] |
Cao Yihua.Principles of helicopter flight dynamics[M].Oxford shire:Coxmoor Publishing Company, 2009
|
[10] |
李国知, 曹义华, 杨倩.纵列式直升机配平计算及稳定性、操纵性分析[J].北京航空航天大学学报, 2009, 35(1): 74- 77 Li Guozhi, Cao Yihua, Yang Qian.Analysis for determiningtrim, stabilityand controllability of tandem helicopter[J].Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(1):74-77(in Chinese)
|