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Expansion of Check-Cases for 6DOF SimulationThis is the Appendix containing a description of the solution for Case 1 in the assessment, “Expansion of Check-Cases for 6DOF Simulation”. For cases of spherical gravity, it is possible to provide a two-body solution without recourse to numerical integration and thus it is accurate to machine precision. Python code for a Keplerian Propagator (propagate.py) which produced a reference trajectory for Case 1 is provided in this appendix. There is also code for generating test cases which was used as an independent verification of the propagator. This is a high-level description of the algorithm employed. The documentation of each function includes implementation details, including equations for each task.
Document ID
20240013559
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Heather M Koehler
(Marshall Space Flight Center Redstone Arsenal, United States)
Matthew J Hawkins
(Marshall Space Flight Center Redstone Arsenal, United States)
Jason R Neuhaus
(Langley Research Center Hampton, United States)
Jesse Couch
(Adaptive Aerospace Group, Inc. Hampton, VA)
Robert L Bossinger
(Adaptive Aerospace Group, Inc. Hampton, VA)
Kyler Brazukas
(Adaptive Aerospace Group, Inc. Hampton, VA)
Trey Fiebelkorn
(Adaptive Aerospace Group, Inc. Hampton, VA)
Edwin Z Crues
(Johnson Space Center Houston, United States)
Benjamin W Margolis
(Ames Research Center Mountain View, United States)
Tristan D Hasseler
(Jet Propulsion Laboratory (JPL))
Justin T Ganiban
(Amentum Chantilly, Virginia, United States)
Nicholas S Olson
(Amentum Chantilly, Virginia, United States)
Zu Qun Li
(Johnson Space Center Houston, United States)
Nathan T Perreau
(Langley Research Center Hampton, United States)
Timothy Curry
(Dynamic Concepts, Inc Redstone Arsenal, United States)
Dane W Erickson
(Marshall Space Flight Center Redstone Arsenal, United States)
Matthew J Andreini
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Zhiqiang Zhou
(Langley Research Center Hampton, United States)
Bruce Jackson
(Adaptive Aerospace Group, Inc. Hampton, VA)
Robert O Shelton
(Johnson Space Center Houston, United States)
Date Acquired
October 25, 2024
Publication Date
October 1, 2024
Publication Information
Subject Category
Astronautics (General)
Report/Patent Number
NESC-RP-23-01853
NASA/TM-20240013031/Volume II/Part 2
Funding Number(s)
WBS: 869021.01.23.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
Modeling
Flight Dynamics
Simulation
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