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X-38 Experimental Controls LawsX-38 Experimental Control Laws X-38 is a NASA JSC/DFRC experimental flight test program developing a series of prototypes for an International Space Station (ISS) Crew Return Vehicle, often called an ISS "lifeboat." X- 38 Vehicle 132 Free Flight 3, currently scheduled for the end of this month, will be the first flight test of a modem FCS architecture called Multi-Application Control-Honeywell (MACH), originally developed by the Honeywell Technology Center. MACH wraps classical P&I outer attitude loops around a modem dynamic inversion attitude rate loop. The dynamic inversion process requires that the flight computer have an onboard aircraft model of expected vehicle dynamics based upon the aerodynamic database. Dynamic inversion is computationally intensive, so some timing modifications were made to implement MACH on the slower flight computers of the subsonic test vehicles. In addition to linear stability margin analyses and high fidelity 6-DOF simulation, hardware-in-the-loop testing is used to verify the implementation of MACH and its robustness to aerodynamic and environmental uncertainties and disturbances.
Document ID
20000039385
Acquisition Source
Johnson Space Center
Document Type
Preprint (Draft being sent to journal)
Authors
Munday, Steve
(NASA Johnson Space Center Houston, TX United States)
Estes, Jay
(NASA Johnson Space Center Houston, TX United States)
Bordano, Aldo J.
(NASA Johnson Space Center Houston, TX United States)
Date Acquired
August 19, 2013
Publication Date
January 1, 2000
Subject Category
Space Transportation And Safety
Report/Patent Number
JSC-CN-6138
Report Number: JSC-CN-6138
Meeting Information
Meeting: Aerospace Control and Guidance Systems Meeting
Location: Lake Tahoe NV
Country: United States
Start Date: March 15, 2000
End Date: March 17, 2000
Sponsors: Society of Automotive Engineers, Inc.
Funding Number(s)
PROJECT: RTOP 487-20-XC-RV
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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