Optimization design of two-layer Walker constellation for LEO navigation augmentation using a dynamic multi-objective differential evolutionary algorithm based on elite guidance-Reference-Cited by-同舟云学术

Optimization design of two-layer Walker constellation for LEO navigation augmentation using a dynamic multi-objective differential evolutionary algorithm based on elite guidance

Published:2022-11-27 Issue:1 Volume:27 Page:
ISSN:1080-5370
Container-title:GPS Solutions
language:en
Short-container-title:GPS Solut

Author:

Deng Zhongliang,Ge Wenxiao^ORCID,Yin Lu,Dai Shisheng

Funder

National Key Project of Research and Development Plan of China

Publisher

Springer Science and Business Media LLC

Subject

General Earth and Planetary Sciences

Link

https://link.springer.com/content/pdf/10.1007/s10291-022-01366-5.pdf

Reference24 articles.

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3. Choy S, Bisnath S, Rizos C (2017) Uncovering common misconceptions in GNSS Precise Point Positioning and its future prospect. GPS Solut 21(1):13–22

4. Deb K, Pratap A, Agarwal S, Meyarivan TAMT (2002) A fast and elitist multi-objective genetic algorithm: NSGA-II. IEEE Trans Evol Comput 6(2):182–197

5. Del Portillo I, Cameron BG, Crawley EF (2019) A technical comparison of three low earth orbit satellite constellation systems to provide global broadband. Acta Astronaut 159:123–135

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