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Assembly Trajectory Planning of Space Telescope Sub-mirror Module Based on Time Optimal Control

  • Hao Ziran
  • , Jiang Zainan*
  • , Li Chongyang
  • , Yang Fan
  • *Corresponding author for this work
  • Harbin Institute of Technology

Research output: Contribution to journalConference articlepeer-review

Abstract

The space telescope stands for the highest level of a nation's aerospace industry, with its manufacturing and launch remaining a worldwide conundrum. The concept of modularized space telescope is proposed herein, the main structure of the sub-mirror module is designed briefly and the assembly scheme of the main telescope is also provided. Besides, the kinematic equation and working conditions of the space robotic arm used for assembly are given, with the cubic B-spline curves formulating the joint space trajectory. Then, with minimizing the moving time as the objective of optimization, displacement, speed and acceleration as the constraint conditions, a mathematical model for time-optimal trajectory planning is established and the genetic algorithm is used to work out solutions. The emulation result shows that the joint space trajectory of the robotic arm obtained on the premise that all the restraint conditions are met can minimize the robotic arm's moving time.

Original languageEnglish
Article number032077
JournalIOP Conference Series: Materials Science and Engineering
Volume439
Issue number3
DOIs
StatePublished - 9 Nov 2018
Event2018 International Conference on Advanced Electronic Materials, Computers and Materials Engineering, AEMCME 2018 - Singapore, Singapore
Duration: 14 Sep 201816 Sep 2018

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