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A modernized approach to meet diversified earth observing system (EOS) AM-1 mission requirementsFrom a flight dynamics perspective, the EOS AM-1 mission design and maneuver operations present a number of interesting challenges. The mission design itself is relatively complex for a low Earth mission, requiring a frozen, Sun-synchronous, polar orbit with a repeating ground track. Beyond the need to design an orbit that meets these requirements, the recent focus on low-cost, 'lights out' operations has encouraged a shift to more automated ground support. Flight dynamics activities previously performed in special facilities created solely for that purpose and staffed by personnel with years of design experience are now being shifted to the mission operations centers (MOCs) staffed by flight operations team (FOT) operators. These operators' responsibilities include flight dynamics as a small subset of their work; therefore, FOT personnel often do not have the experience to make critical maneuver design decisions. Thus, streamlining the analysis and planning work required for such a complicated orbit design and preparing FOT personnel to take on the routine operation of such a spacecraft both necessitated increasing the automation level of the flight dynamics functionality. The FreeFlyer(TM) software developed by AI Solutions provides a means to achieve both of these goals. The graphic interface enables users to interactively perform analyses that previously required many parametric studies and much data reduction to achieve the same result In addition, the fuzzy logic engine enables the simultaneous evaluation of multiple conflicting constraints, removing the analyst from the loop and allowing the FOT to perform more of the operations without much background in orbit design. Modernized techniques were implemented for EOS AM-1 flight dynamics support in several areas, including launch window determination, orbit maintenance maneuver control strategies, and maneuver design and calibration automation. The benefits of implementing these techniques include increased fuel available for on-orbit maneuvering, a simplified orbit maintenance process to minimize science data downtime, and an automated routine maneuver planning process. This paper provides an examination of the modernized techniques implemented for EOS AM-1 to achieve these benefits.
Document ID
19980203782
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Newman, Lauri Kraft
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Hametz, Mark E.
(AI Solutions, Inc. Lanham, MD United States)
Conway, Darrel J.
(AI Solutions, Inc. Lanham, MD United States)
Date Acquired
August 18, 2013
Publication Date
May 1, 1998
Publication Information
Publication: AAS/GSFC 13th International Symposium on Space Flight Dynamics
Volume: 1
Subject Category
Astrodynamics
Report/Patent Number
AAS-98-306
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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