Optics and Precision Engineering, Volume. 18, Issue 1, 100(2010)
Roll stable control and rudder’s technologic parameters of axisymmetric aircrafts
[1] [1] LIU X T. Missile Guidance and Control System Analysis, Design and Simulation [M]. Xi’an:Northwestern Polytechnical University Press, 2006.(in Chinese)
[2] [2] WANG J L, XIE F Q, LIU Y H. The status and development trend of the missile electric steering gear[J]. Winged Missile Journal, 2008,3:42-46. (in Chinese)
[3] [3] WANG G X, HE ZH. Control System Design[M]. Beijing:Tsinghua University Press, 2008. (in Chinese)
[4] [4] LI H W. Servo system of large telescope based on internal model PID control method[J]. Opt. Precision Eng., 2009,2(17):327-332. (in Chinese)
[5] [5] PETER H Z. Modeling and Simulation of Aerospace Vehicle Dynamics[M]. Gainesville: American Institute of Aeronautics and Astronautics,2000.
[6] [6] ZHANG W B, FAN D P, ZHANG ZH Y. Research on application of MEMS gyro to servo system for E-O stabilization and tracking devices[J]. Opt. Precision Eng., 2006,4(14):689-696. (in Chinese)
[7] [7] ZHANG ZH Y , FAN D P, FAN SH X. Servo system design for E-O stabilization and tracking devices[J]. Opt. Precision Eng., 2006,4(14):681-688. (in Chinese)
[8] [8] F. William Nesline, Mark L Nesline. How autopilot requirements constrain the aerodynamic design of homing missiles[C]. American Control conference,America,1984:716-730.
[9] [9] KATSUHIKO. Modern Control Engineering (Fourth Edition)[M]. LU B Y Translated. Beijing:Publishing House of Electronics Industry, 2007. (in Chinese)
[10] [10] QI Z K, XIA Q L. Guided Weapon Control Systems[M]. Beijing: Beijing Institute of Technology,2004.
[11] [11] SALOUA B K, PHILIPPE G, MARE L,et al.. Numerical Simulation of roll induced moment of cruciform tactical missiles[J]. Aerosp. Sci. Technot,2001,5:109-124.
[12] [12] CHEN J SH. Analysis and Design of Missile Guidance and Control System[M].Beijing :China Astronautic Publishing House,1984. (in Chinese)
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ZHANG Yue, DUAN Zhen. Roll stable control and rudder’s technologic parameters of axisymmetric aircrafts[J]. Optics and Precision Engineering, 2010, 18(1): 100
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Received: Jul. 8, 2009
Accepted: --
Published Online: Aug. 31, 2010
The Author Email: Yue ZHANG (zhangyue@ciomp.ac.cn)
CSTR:32186.14.