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Orion Hardware In The Loop OIMU Stimulation Latency Effect on Navigation State EstimationBecause Hardware In The Loop (HITL) testing involves the integration of flight software and flight hardware on the ground, non-flight-like effects may arise. One of these non-flight-like effects includes Inertial Measurement Unit (IMU) stimulation latency that affects the time in which the measurement is received by the Extended Kalman Filter (EKF). This paper seeks to present the extent to which this stimulation latency affects the navigational state estimate from the Orion navigation system for all phases of flight for Artemis II.
Document ID
20250000351
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Christopher A Ertl
(Draper Laboratory Cambridge, Massachusetts, United States)
Robert C Earl
(Lockheed Martin (United States) Bethesda, United States)
Date Acquired
January 11, 2025
Publication Date
January 31, 2025
Publication Information
Publisher: American Astronautical Society
Subject Category
Spacecraft Design, Testing and Performance
Report/Patent Number
AAS-25-151
Meeting Information
Meeting: 47th Annual American Astronautical Society (AAS) Guidance, Navigation and Control (GN&C) Conference
Location: Breckenridge, CO
Country: US
Start Date: January 31, 2025
End Date: February 5, 2025
Sponsors: American Astronautical Society
Funding Number(s)
CONTRACT_GRANT: 80JSC021DA005
CONTRACT_GRANT: 80JSC021F0092
CONTRACT_GRANT: NNJ06TA25C
Distribution Limits
Public
Copyright
Public Use Permitted.
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