跳到主要导航 跳到搜索 跳到主要内容

Dynamics and control for nonideal solar sails around artificial lagrangian points

  • Chuang Yao
  • , Ming Xu*
  • , Tong Luo
  • *此作品的通讯作者
  • Beihang University
  • School of Astronautics

科研成果: 期刊稿件文章同行评审

摘要

Due to their lack of fuel consumption, solar sails have potential applications for deep space exploration. However, due to the optical degradation and deformation of such a sail, a nonideal model is preferable for investigating their dynamics and control when moving around an artificial Lagrangian point. An improved imperfectly reflecting sail model is constructed to compare with the ideal one. With a Hamiltonian structure-preserving controller adopted, the trajectory around an artificial Lagrangian point is generated for ideal solar sails. The original trajectory changes and migrates when the imperfectly reflecting sail model is used. Two improvement strategies are proposed to adjust the changed trajectory. One strategy is to adjust the input parameters of the actuator to compensate for the change in acceleration. The other strategy is to design a new controller to enhance the change and migration of the trajectories. The effectiveness of the two strategies for coping with imperfectly reflecting solar sails is verified via numerical simulations.

源语言英语
页(从-至)575-585
页数11
期刊Journal of Spacecraft and Rockets
55
3
DOI
出版状态已出版 - 2018

学术指纹

探究 'Dynamics and control for nonideal solar sails around artificial lagrangian points' 的科研主题。它们共同构成独一无二的学术指纹。

引用此