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Earth applications orbit analysis for a shuttle-mounted Multispectral MapperThe earth remote sensing problem of orbit design to acquire images with inherent geometric and geodetic accuracy is addressed. The basis for precise orbit modeling is discussed. Various orbit propagation tools are compared. Orbit characteristics for a nominal case at shuttle altitude are displayed. Modeling Parameter sensitivities are evaluated to determine limits on orbit propagation accuracy versus time. It is found that attainable propagation accuracies are sufficient for image quality assessment over the short term at the 15m pixel size desired for a Multispectral Mapper.
Document ID
19810061432
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Driver, J. M.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Tang, C. C. H.
(California Institute of Technology, Jet Propulsion Laboratory, Mission Design Section, Pasadena CA, United States)
Date Acquired
August 11, 2013
Publication Date
August 1, 1981
Subject Category
Earth Resources And Remote Sensing
Report/Patent Number
AAS PAPER 81-182
Report Number: AAS PAPER 81-182
Meeting Information
Meeting: Astrodynamics Specialist Conference
Location: Lake Tahoe, NV
Country: US
Start Date: August 3, 1981
End Date: August 5, 1981
Sponsors: American Astronautical Society, American Institute of Aeronautics and Astronautics
Accession Number
81A45836
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Other

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