@inproceedings{6d99cf66b2bf45c999461eecdb4dc30a,
title = "In-flight calibration of attitude determination systems for information mini-satellites?",
abstract = "Contemporary information mini-satellites have general mass up to 500 kg and are placed onto the orbit altitudes from 500 up to 1500 km. For such spacecraft some principle problems on precise attitude determination and in-ight calibration are considered and elaborated methods are presented for their solving. Original multiple discrete algorithms for filtering, integration and calibration of a strapped-down inertial navigation system for precise determining the spacecraft attitude, are presented. This system contains electrostatic microaccelerometer, an inertial measurement unit based on the gyro sensors, an astronomical system based on star trackers, multi-head Sun sensor and magnetic sensor, the that are fixed to the spacecraft body.",
keywords = "Attitude determination, In-ight calibration, Spacecraft",
author = "Ye Somov and S. Butyrin and H. Siguerdidjane and Ch Hajiyev and V. Fedosov",
year = "2013",
doi = "10.3182/20130902-5-de-2040.00025",
language = "English",
isbn = "9783902823465",
series = "IFAC Proceedings Volumes (IFAC-PapersOnline)",
publisher = "IFAC Secretariat",
number = "PART 1",
pages = "393--398",
booktitle = "19th IFAC Symposium on Automatic Control in Aerospace, ACA 2013 - Proceedings",
edition = "PART 1",
note = "19th IFAC Symposium on Automatic Control in Aerospace, ACA 2013 ; Conference date: 02-09-2013 Through 06-09-2013",
}