Relative Orbit Element Estimation for Satellite Navigation-Reference-Cited by-同舟云学术

Relative Orbit Element Estimation for Satellite Navigation

Published:2005-06-19 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference and Exhibit
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Author:

Doolittle Christina¹,Chavez Frank¹,Lovell Thomas¹

Affiliation:

1. U.S. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-6462

Reference18 articles.

1. Relative-Orbit Element Estimation for Satellite Navigation and Guidance

2. F. Bauer et al, "Satellite Formation Flying Using an Innovative Autonomous Control System (AUTOCON) Environment," AIAA Paper 97-3821, presented at the AIAA Guidance, Navigation,andControlConference,Aug.1997.

3. Satellite Formation Flying Design and Evolution

4. D. W. Gim and K. T. Alfriend, "The State Transition Matrix of Relative Motion for the Perturbed Non-Circular Reference Orbit," AAS Paper 01-222, presented at the AAS/AIAA SpaceFlightMechanicsMeeting,SantaBarbara,CA,Feb11-16,2001.

5. R. Howard and T. Storch, "Delta-V Requirements for Staring and Expedient Circular Circumnavigation",AIAASpace2001Conference,Albuquerque,NM,AIAAPaper01-4740.

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Determination and Estimation of Differential Mean Orbital Elements for Formation-Flying Missions;Journal of Guidance, Control, and Dynamics;2014-01

2. Relative Orbital Element Estimation and Observability Analysis for Formation Flying Satellites using Inter-Satellite Range Measurements Only;AIAA Guidance, Navigation, and Control Conference;2010-06-26