Analytic LQR Design for Spacecraft Control System Based on Quaternion Model

@inproceedings{Yang2012AnalyticLD,
  title={Analytic LQR Design for Spacecraft Control System Based on Quaternion Model},
  author={Yaguang Yang},
  year={2012}
}
AbstractIn this paper, linear-quadratic regulator (LQR) method is proposed for the design of nonlinear spacecraft control systems. The proposed design is based on the linearized spacecraft model that involves only three components of the quaternion. By using a simple and special structure of the linearized reduced quaternion model, an analytical solution for the controller. It is shown that the analytical solution of the state feedback matrix is an explicit function of the cost matrices Q and R… CONTINUE READING

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