Providing of the functional stability of the spacecraft’s orientation and stabilization

Authors

  • Сергей Николаевич Фирсов National Aerospace University “Kharkov Aviation Institute” Str. Chkalov 17, Kharkov, 61070, Ukraine

DOI:

https://doi.org/10.15587/2313-8416.2014.26399

Keywords:

failure, stability restoration, angular velocity sensor, flywheels engines, stabilization and orientation satellite system, functional stability, measuring unit

Abstract

The tools for diagnosis and restoring the functionality of the orientation and stabilization systems are presented. The software system for debugging modules providing functional stability and algorithmic support is described.  One of the possible solutions to scientific and applied task of providing the functional stability of stabilization systems and aircraft orientation is given. The criteria, the fulfillment of which provides a functional sustainability are determined.

Author Biography

Сергей Николаевич Фирсов, National Aerospace University “Kharkov Aviation Institute” Str. Chkalov 17, Kharkov, 61070

Ph.D., associate professor, doctoral

Chair of aircraft control systems

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Published

2014-08-13

Issue

Section

Technical Sciences