In-flight Management for Attitude Control System with Animation of Satellite Motion

Ye Somov; S. Butyrin; S. Somov; T. Somova; C. Hajiyev; V. Sukhanov

doi:10.1016/j.ifacol.2016.07.878

In-flight Management for Attitude Control System with Animation of Satellite Motion

Ye Somov, S. Butyrin, S. Somov, T. Somova, C. Hajiyev, V. Sukhanov

Department of Aeronautical Engineering

Research output: Contribution to journal › Article › peer-review

2 Citations (Scopus)

Abstract

Contemporary land-survey satellites are placed onto the orbit altitudes from 600 up to 1000 km. For such spacecraft we consider some principal problems on the spacecraft attitude digital and pulse-width control and present elaborated methods for in-flight identification, verification and management of attitude control system with animation of satellite motion.

Original language	English
Pages (from-to)	833-838
Number of pages	6
Journal	IFAC-PapersOnLine
Volume	49
Issue number	12
DOIs	https://doi.org/10.1016/j.ifacol.2016.07.878
Publication status	Published - 2016

Bibliographical note

Publisher Copyright:
© 2016

Keywords

attitude control system
in-flight management
land-survey satellite

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10.1016/j.ifacol.2016.07.878

Cite this

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title = "In-flight Management for Attitude Control System with Animation of Satellite Motion",

abstract = "Contemporary land-survey satellites are placed onto the orbit altitudes from 600 up to 1000 km. For such spacecraft we consider some principal problems on the spacecraft attitude digital and pulse-width control and present elaborated methods for in-flight identification, verification and management of attitude control system with animation of satellite motion.",

keywords = "attitude control system, in-flight management, land-survey satellite",

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language = "English",

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AU - Somov, Ye

AU - Butyrin, S.

AU - Somov, S.

AU - Somova, T.

AU - Hajiyev, C.

AU - Sukhanov, V.

PY - 2016

Y1 - 2016

N2 - Contemporary land-survey satellites are placed onto the orbit altitudes from 600 up to 1000 km. For such spacecraft we consider some principal problems on the spacecraft attitude digital and pulse-width control and present elaborated methods for in-flight identification, verification and management of attitude control system with animation of satellite motion.

AB - Contemporary land-survey satellites are placed onto the orbit altitudes from 600 up to 1000 km. For such spacecraft we consider some principal problems on the spacecraft attitude digital and pulse-width control and present elaborated methods for in-flight identification, verification and management of attitude control system with animation of satellite motion.

KW - attitude control system

KW - in-flight management

KW - land-survey satellite

UR - https://www.scopus.com/pages/publications/84992342867

U2 - 10.1016/j.ifacol.2016.07.878

DO - 10.1016/j.ifacol.2016.07.878

M3 - Article

AN - SCOPUS:84992342867

SN - 2405-8963

VL - 49

SP - 833

EP - 838

JO - IFAC-PapersOnLine

JF - IFAC-PapersOnLine

IS - 12

ER -

In-flight Management for Attitude Control System with Animation of Satellite Motion

Abstract

Bibliographical note

Keywords

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