Federated nonlinear predictive filtering for the gyroless attitude determination system
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- 作者：Lijun Zhanga ; b ; c ; alijun_007@163.com" class="auth_mail" title="E-mail the corresponding author ; alijun@nudt.edu.cn" class="auth_mail" title="E-mail the corresponding author ; Shan Qiana ; shanqian_123@163.com" class="auth_mail" title="E-mail the corresponding author ; Shifeng Zhangb ; zhang_shifeng@hotmail.com" class="auth_mail" title="E-mail the corresponding author ; Hong Caib ; hcai@nudt.edu.cn" class="auth_mail" title="E-mail the corresponding author
- 关键词：Gyroless spacecraft ; Federated filter ; Nonlinear predictive filter ; Attitude determination
- 刊名：Advances in Space Research
- 出版年：2016
- 出版时间：1 November 2016
- 年：2016
- 卷：58
- 期：9
- 页码：1671-1681
- 全文大小：990 K
文摘
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A federated NPF for the gyroless attitude determination system with star sensor and GPS sensor is presented.
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This approach combines the good qualities of both the NPF and federated filter.
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A fault detection and isolation algorithm is applied to the proposed federated NPF.