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This file was created with JabRef 2.1 beta 2.
Encoding: GB2312
@misc{Zarchan2013Tactical,
note = {ZARCHAN P. Tactical and strategic missile guidance[M]. 6th ed. Reston: AIAA, 2012: 35-105.},
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@misc{NESLINE1981Anew,
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@misc{He2017A,
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@misc{Wang2007Status,
note = {王亚飞, 方洋旺, 周晓滨. 比例导引律研究现状及其发展[J]. 火力与指挥控制, 2007, 32(10): 8-12.\\
WANG Y F, FANG Y W, ZHOU X B. The status quo of proportional navigation guidance law and its development[J]. Fire Control and Command Control, 2007, 32(10): 8-12(in Chinese).},
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@misc{Chen2009Guidance,
note = {陈峰, 肖业伦, 陈万春. 基于零控脱靶量的大气层外超远程拦截制导[J]. 航空学报, 2009, 30(09): 1583-1589.\\
CHEN F, XIAO Y L, CHEN W C. Guidance based on zero effort miss for super-range exoatmospheric intercept[J]. Acta Aeronautica Et Astronautica Sinica, 2009, 30(09): 1583-1589(in Chinese).},
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@misc{Chen2008Velocity,
note = {陈峰, 王育林, 肖业伦等. 基于预测脱靶量的远程拦截速度增益导引[J]. 航空学报, 2008, 29(06): 1665-1672.\\
CHEN F, WANG Y L, XIAO Y L, et al. Velocity-to-be-gained guidance based on predicted miss distance for long-range intercept[J]. Acta Aeronautica Et Astronautica Sinica, 2008, 29(06): 1665-1672(in Chinese).},
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@misc{Su2016Novel,
note = {SU W S, YAO D N, LI K B, et al. A novel biased proportional navigation guidance law for close approach phase[J]. Chinese Journal of Aeronautics, 2016, 29(01): 228-237.},
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@misc{Yu2016Optimal,
note = {YU W B, CHEN W C, YANG L, et al. Optimal terminal guidance for exoatmospheric interception[J]. Chinese Journal of Aeronautics, 2016, 29(04): 1052-1064.},
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@misc{Weiss2005Adjoint,
note = {WEISS M. Adjoint method for missile performance analysis on state-space models[J]. Journal of Guidance Control and Dynamics, 2005, 28(2): 236-248.},
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@misc{CODDINGTON1955Theory,
note = {CODDINGTON E A, LEVINSON N. Theory of ordinary differential equations[M]. New York: McGraw-Hill Book Company, Inc., 1955: 108-137.},
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@misc{Domb1957susceptibility,
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@misc{Wang2013Time,
note = {王辉, 林德福, 祁载康等. 时变最优的增强型比例导引及其脱靶量解析解[J]. 红外与激光工程, 2013, 42(03): 692-698.\\
WANG H, LIN D F, QI Z K, et al. Time-varying optimal augmented proportional navigation and miss distance closed-form solutions[J]. Infrared and Laser Engineering, 2013, 42(03): 692-698(in Chinese).},
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@misc{Ascher2011first,
note = {ASCHER, U, GREIF C. A first course in numerical methods[M]. Philadelphia: Society for Industrial and Applied Mathematics, 2011: 35-55.},
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@misc{Higham2002Accuracy,
note = {HIGHAM N. Accuracy and stability of numerical algorithms[M]. 2nd ed. Philadelphia: Society for Industrial and Applied Mathematics, 2002: 93-104.},
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@misc{He2018Adjoint,
note = {赫泰龙, 陈万春, 刘芳. 高超声速飞行器平稳滑翔扰动运动伴随分析[J/OL]. 北京航空航天大学学报,(2018-04-18)[2018-04-20]. http://kns.cnki.net/kcms/detail/11.2625.V.20180418.1057.003.html\\
HE T L, CHEN W C, LIU F. Adjoint analysis of steady glide with disturbance motion for hypersonic vehicle[J/OL]. Journal of Beijing University of Aeronautics and Astronautics,(2018-04-18)[2018-04-20]. http://kns.cnki.net/kcms/detail/11.2625.V.20180418.1057.003.html},
}