Nonlinear Augmented Proportional Navigation for Midrange Rendezvous Guidance and Performance Assessment
Guidance systems are important to autonomous rendezvous with uncooperative targets such as an active debris removal (ADR) mission. A novel guidance frame is established in rotating line-of-sight (LOS) coordinates, which resolves the coupling effect between pitch and yaw planes in a general 3D scenar...
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| Format: | Article |
| Language: | English |
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Wiley
2019-01-01
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| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/2019/1725629 |
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| _version_ | 1832554574424047616 |
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| author | Weilin Wang Xumin Song |
| author_facet | Weilin Wang Xumin Song |
| author_sort | Weilin Wang |
| collection | DOAJ |
| description | Guidance systems are important to autonomous rendezvous with uncooperative targets such as an active debris removal (ADR) mission. A novel guidance frame is established in rotating line-of-sight (LOS) coordinates, which resolves the coupling effect between pitch and yaw planes in a general 3D scenario. The guidance law is named augmented proportional navigation (APN) by applying nonlinear control along LOS and classical proportional navigation normal to LOS. As saving time is a critical factor in space rescue and on-orbit service, the finite time convergence APN (FTCAPN) is further proposed which proves to possess convergence and high robustness. This paper builds on previous efforts in polynomial chaos expansion (PCE) to develop an efficient analysis technique for guidance algorithms. A large scope of uncertainty sources are considered to make state evaluation trustworthy and provide precise prediction of trajectory bias. The simulation results show that the accuracy of the proposed method is compatible with Monte Carlo simulation which requires extensive computational effort. |
| format | Article |
| id | doaj-art-7df71221dfc04da0bf8d35482842c281 |
| institution | Kabale University |
| issn | 1687-5966 1687-5974 |
| language | English |
| publishDate | 2019-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | International Journal of Aerospace Engineering |
| spelling | doaj-art-7df71221dfc04da0bf8d35482842c2812025-02-03T05:51:07ZengWileyInternational Journal of Aerospace Engineering1687-59661687-59742019-01-01201910.1155/2019/17256291725629Nonlinear Augmented Proportional Navigation for Midrange Rendezvous Guidance and Performance AssessmentWeilin Wang0Xumin Song1Space Engineering University, Beijing 100014, ChinaSpace Engineering University, Beijing 100014, ChinaGuidance systems are important to autonomous rendezvous with uncooperative targets such as an active debris removal (ADR) mission. A novel guidance frame is established in rotating line-of-sight (LOS) coordinates, which resolves the coupling effect between pitch and yaw planes in a general 3D scenario. The guidance law is named augmented proportional navigation (APN) by applying nonlinear control along LOS and classical proportional navigation normal to LOS. As saving time is a critical factor in space rescue and on-orbit service, the finite time convergence APN (FTCAPN) is further proposed which proves to possess convergence and high robustness. This paper builds on previous efforts in polynomial chaos expansion (PCE) to develop an efficient analysis technique for guidance algorithms. A large scope of uncertainty sources are considered to make state evaluation trustworthy and provide precise prediction of trajectory bias. The simulation results show that the accuracy of the proposed method is compatible with Monte Carlo simulation which requires extensive computational effort.http://dx.doi.org/10.1155/2019/1725629 |
| spellingShingle | Weilin Wang Xumin Song Nonlinear Augmented Proportional Navigation for Midrange Rendezvous Guidance and Performance Assessment International Journal of Aerospace Engineering |
| title | Nonlinear Augmented Proportional Navigation for Midrange Rendezvous Guidance and Performance Assessment |
| title_full | Nonlinear Augmented Proportional Navigation for Midrange Rendezvous Guidance and Performance Assessment |
| title_fullStr | Nonlinear Augmented Proportional Navigation for Midrange Rendezvous Guidance and Performance Assessment |
| title_full_unstemmed | Nonlinear Augmented Proportional Navigation for Midrange Rendezvous Guidance and Performance Assessment |
| title_short | Nonlinear Augmented Proportional Navigation for Midrange Rendezvous Guidance and Performance Assessment |
| title_sort | nonlinear augmented proportional navigation for midrange rendezvous guidance and performance assessment |
| url | http://dx.doi.org/10.1155/2019/1725629 |
| work_keys_str_mv | AT weilinwang nonlinearaugmentedproportionalnavigationformidrangerendezvousguidanceandperformanceassessment AT xuminsong nonlinearaugmentedproportionalnavigationformidrangerendezvousguidanceandperformanceassessment |