Energy-Orientational Approach to Identification of Errors of Inertial Measurements in Inertial Satellite Control Systems
The suggested approach to the identification of errors is based on the following: – on the transition from the space of the full movement parameters that include ground-supported (satellite) trajectory measurements to the space of the apparent parameters that include the unknown errors; – on the properties of the error observability individual for every their type appearing in different ways on different types of movement; – on the decomposition of the errors appearing in the orientation errors of the vector of the apparent developed speed and in the errors of the energy accumulated in the module of its vector.