NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
IMUFDIR Tuning In Response To Structural Deformation Of The Orion CapsuleDuring system level Thermal Vacuum (TVAC) testing it was discovered that the pressure differential of the crew cabin in a vacuum would deflect the capsule slightly, causing significant misalignment of Orion’s three Inertial Measurement Units (IMUs). This phenomenon has been likened to a balloon expanding. When this misalignment was modeled in simulation as a function of atmospheric pressure, it was determined that the rate of deflection on reentry was significant enough to cause a mis-compare of the angular rates measured by the IMUs. This mis-comparison of the rates caused Orion’s Fault Detection Isolation and Recovery (FDIR) algorithm to falsely fail one of the IMUs. This manuscript will discuss how the IMUFDIR algorithm was detuned to be insensitive to these ballooning effects, while still meeting FDIR requirements to capture real faults in an IMU. All testing to validate this detuning was performed in a Six Degree of Freedom (6 DOF) Monte Carlo Simulation Environment.
Document ID
20220000085
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Nicholas Rahaim
(Lockheed Martin (United States) Bethesda, Maryland, United States)
Brandon Wood
(Johnson Space Center Houston, Texas, United States)
Date Acquired
January 18, 2022
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: 44th Annual AAS Guidance, Navigation and Control (GN&C) Conference
Location: Breckenridge, CO
Country: US
Start Date: February 3, 2022
End Date: February 9, 2022
Sponsors: American Astronautical Society
Funding Number(s)
WBS: 747797.06.13.15.99.10
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
Single Expert
No Preview Available