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An end-to-end pointing budget approach to planetary observing systems with application to EOSPreviously published error budgets have focused on spacecraft error sources for pointing error and have tended to include only spacecraft pointing rather than the ultimate geolocation of each pixel of dam onto a well-defined spot on the surface of the Earth. A systematic approach to geolocation error budgeting, including all contributors in the geolocation process is presented. Its structure allows simultaneous expression of the needs of instrument teams as well as spacecraft design teams. It allows explicit acknowledgement of approximations made for on-board control as well as the ultimate geolocation accuracy achievable after ground processing and exploits the commonality inherent in the on-board and post-processing error budgets. It also includes the uncontrolled and unmeasured spacecraft jitter. This approach can be used to investigate the mission-wide benefit of a variety of design choices, (such as on-board sensing and ground correction of measurements contrasted with on-board correction of measurements). Additionally, in light of increasing accuracy requirements as sensor resolution improves, numerous non-spacecraft contributors to geolocation error are quantified.
Document ID
19930046922
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Throckmorton, A.
(McDonnell Douglas Aerospace Seabrook, MD, United States)
Date Acquired
August 16, 2013
Publication Date
February 1, 1993
Subject Category
Spacecraft Instrumentation
Report/Patent Number
AIAA PAPER 93-1005
Meeting Information
Meeting: AIAA, AHS, and ASEE, Aerospace Design Conference
Location: Irvine, CA
Country: United States
Start Date: February 16, 1993
End Date: February 19, 1993
Sponsors: AIAA, ASEE, AHS
Accession Number
93A30919
Funding Number(s)
CONTRACT_GRANT: NAS5-30363
Distribution Limits
Public
Copyright
Other

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