NASA NTRS · 19740004242
Strapdown system Performance Optimization Test evaluations (SPOT), volume 2
Abstract
A three axis inertial system is packaged in an Apollo gimbal fixture for fine grain evaluation of strapdown system performance in dynamic environments. These evaluations have provided information to assess the effectiveness of real-time compensation techniques and to study system performance tradeoffs to factors such as quantization iteration rate. The strapdown performance and tradeoff studies conducted in this program are discussed.
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Blaha, R. J., Gilmore, J. P.. 1973-02-01. Strapdown system Performance Optimization Test evaluations (SPOT), volume 2. https://ntrs.nasa.gov/citations/19740004242
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