YI Zhong-gui, GE Xin-sheng. Optimal Attitude Control of Underactuated Spacecrafts With the Gauss Pseudospectral Method[J]. Applied Mathematics and Mechanics, 2017, 38(12): 1319-1330. doi: 10.21656/1000-0887.380013
Citation: YI Zhong-gui, GE Xin-sheng. Optimal Attitude Control of Underactuated Spacecrafts With the Gauss Pseudospectral Method[J]. Applied Mathematics and Mechanics, 2017, 38(12): 1319-1330. doi: 10.21656/1000-0887.380013

Optimal Attitude Control of Underactuated Spacecrafts With the Gauss Pseudospectral Method

doi: 10.21656/1000-0887.380013
Funds:  The National Natural Science Foundation of China(11472058)
  • Received Date: 2017-01-10
  • Rev Recd Date: 2017-02-20
  • Publish Date: 2017-12-15
  • The attitude and orientation of modern spacecrafts generally can be controlled by 3 orthogonal reaction momentum wheels. The attitude control of underactuated spacecrafts with only 2 momentum wheels and failed out of complete 3-axis controlling torques, was investigated. The control problem was converted to a nonholonomic motion planning problem of a drift-free system with zero angular momentum. The attitude motion planning problem of a spacecraft with 2 momentum wheels was converted to a nonlinear programming problem (NLP) with the Gauss pseudospectral method, and then solved with the SQP algorithm. Through numerical simulation the optimal control met the design requirements of zero boundaries, so the wheels can be controlled easily by servomotors; the planned attitude curves were almost identical to the numerically integrated solutions; the number of suitable collocation points was found through balancing among 3 factors: the target function value, the running time and the solution error. The results show that the proposed method is effective for the optimal attitude control of underactuated spacecrafts.
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