Microaccelerations on Board Earth Artificial Satellites. Analysis and Use of Measurement Data Received from on Board Accelerometers

The following problems arising in analysis and use of data received from Space Acceleration Measurement System (SAMS) are considered: 1) calculating a quasi-state acceleration component on the base of information about real satellite attitude motion, using this component for testing accelerometers in a low frequency range; 2) spectral analysis of measurement data obtained in the Space Shuttle STS-60 mission and on board the Mir orbital station; 3) digital filtering and approximating a low frequency acceleration component.