A previously developed method is used to evaluate the error in the optical passive ring-resonator gyro. This scheme is shown to have sufficient accuracy to meet high-grade aircraft-navigation requirements with enough tolerance for such resonator parameters as splice misalignment, finesse, and temperature.>
No takes yet. Share an insight, caveat, or question.
Takiguchi et al. (1991) studied this question.
Synapse has enriched 5 related papers. Consider them for comparative context: