SU Yuan, CAO Yi-hua. Dynamic Stability Analysis and Control Law Design of Stability Augmentation System for Helicopter[J]. Journal of Beijing University of Aeronautics and Astronautics, 2002, 28(6): 636-639. (in Chinese)
Citation: SU Yuan, CAO Yi-hua. Dynamic Stability Analysis and Control Law Design of Stability Augmentation System for Helicopter[J]. Journal of Beijing University of Aeronautics and Astronautics, 2002, 28(6): 636-639. (in Chinese)

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

  • Received Date: 23 Apr 2001
  • Publish Date: 30 Jun 2002
  • Dynamic stability and control laws of a hingeless rotor helicopter were studied. Based on dynamic stability analysis of the helicopter, the unstable mode and the necessity of installation of Stability Augmentation System (SAS) were cognized. The control laws of SAS for helicopter pitching, rolling and yawing motions were presented. Following establishing helicopter flight control state equations, the calculations of effective derivatives, the performance analysis and step response simulation for helicopter SAS were carried out. Through the design of SAS, the helicopter dynamic stability can be improved, the stability augmentation performance can meet the requirements of the first level qualities of the design specifications.

     

  • [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.
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