VESTNIK of Samara University. Aerospace and Mechanical EngineeringVESTNIK of Samara University. Aerospace and Mechanical Engineering2542-04532541-7533Samara National Research University225010.18287/2541-7533-2012-0-4(35)-29-37UnknownImprovement of the flight attitude control accuracy of the Earth observation spacecraftAkhmetovR. N.<p>Doctor of Engineering Science</p>
<p>General Designer</p>csdb@samspace.ruSollogubA. V.<p>Doctor of Engineering Science</p>
<p>Chief Scientific Adviser</p>csdb@samspace.ruMakarovV. P.<p>Doctor of Engineering Science</p>
<p>Scientific Adviser</p>csdb@samspace.ruGolovchenkoA. A.<p>Leading Design Engineer</p>csdb@samspace.ruFilatovA. V.<p>Leading Design Engineer</p>csdb@samspace.ruSpace Rocket Center “TsSKB-Progress”, Samara1812201211429370203201502032015Copyright © 2015, VESTNIK of the Samara State Aerospace University2015<p>The paper presents the problems of assessing the relative position of angular accelerometer sensitivityaxes and astromeasuring basis of the attitude control system as part of flight calibration of a platformindependentinertial system. The inaccuracy of the angular accelerometer is defined and taken into account. Analgorithm of in-flight geometrical and parametric calibration of the meter is suggested.</p>Angular accelerometergeometrical and parametric calibrationrelative position of axesastromeasuring basisonboard equipmentattitude control systemИзмеритель угловой скоростигеометрическая и параметрическая полётная калибровкавзаимное положение осейастроизмерительный базисбортовая аппаратурасистема управления ориентацией