Dynamic Stability Analysis and Control Law Design of Stability Augmentation System for Helicopter

[1] Johnson W. Helicopter Theory[M]. New Jersey:Princeton University Press,1980. [2]Hess R A,Gao C. A generalized algorithm for inverse simulation applied to helicopter maneuvering flight [J]. Journal of the American Helicopter Society, 1993, 38(4):3~15. [3]Cao Yihua. A new inverse solution technique for studying helicopter maneuvering flight[J]. Journal of the American Helicopter Society, 2000, 45(1):43~53. [4]Curtiss H C, Shup N K. A stability and control theory for hingeless rotor helicopter . Proceedings of the 27th Annual Forum of the American Helicopter Society . 1971. [5]Bramwell A R S. A method for calculating the stability and control derivatives of helicopter with hingeless rotor . RM, AERO 69/4, London:the City Univ, 1970. [6]Keller J D. An investigation of helicopter dynamic coupling using an analytical model . 21th European Rotorcraft Forum . 1995. [7]Wang S, Xu Z. A simplified method for predicting rotor blade airloads . Seventh European Rotorcraft and Power Lift Aircraft Forum . 1981. [8]Cao Yihua. A new method for predicting rotor wake geometries and downwash velocity field[J]. Aircraft Engineering and Aerospace Technology:An International Journal, 1999, 71(2):129~135. [9]Reichert G, Oelker P. Handling qualities with the Bolkow rigid rotor system . Proceeding of the 24th Annual National Forum of the A H S .1968. [10]Biggers J C, Mccloud J L,Patterakis P. Wind tunnel test of two full scale helicopter fuselages . NASA TND-1548, 1962. [11]Rix O, Huber H, Kaleka J. Parameter identification of a hingeless rotor helicopter . Proceeding of the 33th Annual National Forum of the A H S . 1977. [12]GJB 3216-98 直升机增稳系统通用规范[S].北京:国防工业出版社,1998.