Formation Flight for Close Satellites With GPS-Based State Estimation Method
Author:
Affiliation:
1. Hezarfen Aeronautics and Space Technologies Institute, Turkish National Defence University, İstanbul, Turkey
2. Faculty of Aeronautics and Astronautics, Istanbul Technical University, İstanbul, Turkey
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Subject
Electrical and Electronic Engineering,Instrumentation
Link
http://xplorestaging.ieee.org/ielx7/7361/9845438/09807648.pdf?arnumber=9807648
Cited by 4 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. A Data-Driven Interval Type-2 Fuzzy Kalman Filter of Minimum Realization for Forecasting Spacecraft Formation on Low Earth Orbit;Global Perspectives on Robotics and Autonomous Systems;2023-06-16
2. Estimation of the Relative States of Satellite Formation Flights Using the Adaptive Extended Kalman Filter;Gyroscopy and Navigation;2023-06
3. Fault-tolerant state estimation methods of cluster satellites;Advances in Space Research;2023-05
4. Relative Orbital Motion Control of Spacecraft Based on Multi-Objective Optimization;Aerospace;2023-01-31
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