Conventional accelerometer orientations obtain only a portion of the system performance available from the accelerometers. Therefore, the use of optimum nonorthogonal and redundant accelerometer orientations can result in significantly improved performance. This paper develops a general formulation of the accelerometer orientation optimization problem, presents solutions for certain special cases, and includes the results of examples to demonstrate the potential of non-conventional orientations.
Optimizing Accelerometer Orientations
Sae Technical Papers
NASA Aerospace Vehicle Flight Control Conference ; 1965
1965-02-01
Conference paper
English
Optimizing accelerometer orientations
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