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pro vyhledávání: '"Spencer, David"'
Autor:
Spencer, David Allen
This dissertation develops a methodology for automated trajectory control of a spacecraft about a non-maneuvering target. The methodology utilizes relative orbital elements (ROEs), combined with guidance laws based upon artificial potential functions
Externí odkaz:
http://hdl.handle.net/1853/53549
Autor:
Spencer, David Ian.
Thesis (Ph. D.)--University of California, Davis, 2009.
Title based on PDF title page (viewed 06/10/2010). Degree granted in Philosophy.
Title based on PDF title page (viewed 06/10/2010). Degree granted in Philosophy.
Externí odkaz:
http://proquest.umi.com/pqdweb?did=1987416841&sid=1&Fmt=2&clientId=48051&RQT=309&VName=PQD
Publikováno v:
In Acta Astronautica September 2024 222:661-673
Publikováno v:
In The Journal of Space Safety Engineering March 2024 11(1):120-126