NASA NTRS · 19720000623
Computer program to generate attitude error equations for a gimballed platform
Abstract
Computer program for solving attitude error equations related to gimballed platform is described. Program generates matrix elements of attitude error equations when initial matrices and trigonometric identities have been defined. Program is written for IBM 360 computer.
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Hall, W. A., Jr., Morris, T. D., Rone, K. Y.. 1972-10-01. Computer program to generate attitude error equations for a gimballed platform. https://ntrs.nasa.gov/citations/19720000623
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