期刊文献+

基于自适应Radau伪谱法的再入段轨道设计算法 被引量:1

The Re-Entry Orbit Design Algorithm Based on an Adaptive Radau Pseudo-Spectral Method
下载PDF
导出
摘要 针对传统Radau伪谱法处理非光滑平面时精度不高和效率不足的缺点,提出了一种基于自适应Radau伪谱算法的再入段轨道设计算法.该算法可以根据状态方程的拟合精度对再入段轨道进行自适应调整.在轨道曲率较高的区域,通过增加区段数量提高计算精度;在轨道曲率较低的区域,通过提高插值多项式的阶次提高计算精度.仿真结果显示,该算法形成的配点分布更为合理,相对传统的Radau算法具有高精度、高效率等优点,求解效果优于传统的Radau伪谱法,可将其应用到再入段轨道优化的工程实际中. To solve the problems of low accuracy and poor efficiency of the traditional Radau pseudo-spectral method in dealing with non-smooth surfaces,an adaptive Radau pseudo-spectral method was proposed to generate the optimal re-entry orbit.The algorithm could adjust the intervals adaptively according to the approximation precision of state equations.In regions of relatively high curvature,the accuracy was increased by dividing a segment into more mesh intervals,whereas in regions of relatively low curvature,accuracy was increased by increasing the degree of the approximating polynomial within a mesh interval.Simulation results show that the nodes distribution generated by the adaptive Radau pseudo-spectral re-entry orbit design algorithm is more reasonable and efficient than that of the traditional Radau pseudo-spectral method.The algorithm can be applied to re-entry orbit design in practical engineering due to its high efficiency and high precision.
作者 张恒浩 ZHANG Heng-hao(R&D Center,China Academy of Launch Vehicle Technology,Beijing 100076,China)
出处 《北京理工大学学报》 EI CAS CSCD 北大核心 2018年第10期1037-1045,共9页 Transactions of Beijing Institute of Technology
基金 国家预研资助项目(513201102)
关键词 拉格朗日插值 优化 再入轨道 Radau伪谱法 轨道计算 Lagrange interpolation optimization re-entry orbit Radau pseudo-spectral method orbit computing
  • 相关文献

参考文献6

二级参考文献27

  • 1于明礼,文浩,胡海岩,赵永辉.二维翼段颤振的μ控制[J].航空学报,2007,28(2):340-343. 被引量:15
  • 2Xue S B, Lu P. Constrained predictor-corrector entry guidance [J]. Journal of Guidance, Control, and Dynamics, 2010, 33 (4) : 1273 -1281.
  • 3Roenneke A J, Cornwell P J. re-entry vehicle [ J ]. Journal Dynamics, 1993, 16(5) : 927 - Trajectory control for a low-lift of Guidance, Control, and 933.
  • 4南英.航天飞机再入抗干扰轨道优化设计[D].西安:西北工业大学,1990.
  • 5Lu P. Regulation about time-varying trajectories: precision entry guidance illustrated [ J ]. Journal of Guidance, Control, and Dynamics, 1999, 22 (6) : 784 - 790.
  • 6Tian B L, Zong Q. Optimal guidance for reentry vehicles based on indirect legendre pseudospectral method [ J ]. Acta Astronautica, 2011, 68(7): 1176-1184.
  • 7Zhou H, Tawfiqur R, Wang D W, et al. Onboard pseudospectral guidance for re-entry vehicle [ J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2014, 228 ( 11 ) : 1925 - 1936.
  • 8Yan H, Fahroo F, Ross I M. Optimal feedback control laws by legendre pseudospectral approximations [ C ]. The American Control Conference, Arlington, USA, June 25 - 27, 2001.
  • 9Phillips T H. A common aero vehicle (CAV) model description and employment guide [ R ]. Schafer Corporation for AFRL and AFSPC, 2003.
  • 10Garg D, Patterson M A, Darby C L, et al. Direct trajectory optimization and costate estimation of finite-horizon and infinite- horizon optimal control problems using a Radau Pseudospectral Method [ J ]. Computational Optimization and Applications, 2011, 49(2) : 335 -358.

共引文献78

同被引文献26

引证文献1

二级引证文献2

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部