The problems on synthesis of the guidance laws and algorithms for digital attitude control for an observation spacecraft at the areal geodetic surveying are considering. The land-surveying is carried out by a set of extended orthodromic routes of scanning optoelectronic observation for a given part of the Earth surface. Results on the efficiency of the developed vector guidance laws, algorithms for discrete filtering and digital gyromoment control of a satellite orientation during the areal surveying from sun-synchronous orbit are presented.
Satellite guidance and attitude control during the areal geodetic surveying
ICNPAA 2018 WORLD CONGRESS: 12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences ; 2018 ; Yerevan, Armenia
AIP Conference Proceedings ; 2046 , 1
2018-12-04
10 pages
Conference paper
Electronic Resource
English
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