Model-free self-adaptive control method for attitude of assembled spacecraft

Model-free self-adaptive control method for attitude of assembled spacecraft

  • CN 105,912,013 A
  • Filed: 07/04/2016
  • Published: 08/31/2016
  • Est. Priority Date: 07/04/2016
  • Status: Active Application
First Claim
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1. an assembly spacecraft attitude MFA control method, it is characterised in that comprise following stepRapid:

  • S1, for the attitude motion of general assembly spacecraft, sets up full format dynamic equivalence linearData model, determines the pseudo-gradient vector form in this model;

    S2, for the pseudo-gradient vector in full format dynamic equivalence linear data model, design parameterART network equation, estimates pseudo-gradient vector;

    S3, sets up error rule function according to dynamic equivalence linear data model, by minimizing by mistakeDifference criterion function designs weighting one step controller forward.

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