Providing of the functional stability of the spacecraft’s orientation and stabilization
DOI:
https://doi.org/10.15587/2313-8416.2014.26399Keywords:
failure, stability restoration, angular velocity sensor, flywheels engines, stabilization and orientation satellite system, functional stability, measuring unitAbstract
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.
References
Sevastyanov ,N. N. (2009). Analysis of current opportunities to create small space up preparations for remote sensing. PROCEEDINGS MIPT, 1 (3), 14–22.
Kulik, A. S., Luchenko, O. A., Firsov, S. N. (2011). The concept of survivability of satellite attitude control systems and stabilization. Journal of Radіoelektronіka, іnformatika, upravlіnnya, 2 (25), 47–41.
Firsov, S. N. (2013). Complex indices of functional stability SAT stabilization systems and orientation. Journal of Aerospace and Technology, 1 (98), 31–38.
Firsov, S. N. (2014). Forming of fault–tolerant flywheel engine blocks in satellite systems of orientation and stabilization. Journal of Computer and Systems Sciences International, 4 (53), 601–609.
Firsov, S. N. (2013). Formation of a stable fault structure measuring motion parameters teley orientation and stabilization systems. Journal of Gyroscopes and Navigation, 4 (83), 72–83.
Reznikova, O., Firsov, S. (2013). Fuzzy Resource Selection for the Functional State Re– covery of the Fault System. East West Fuzzy Colloquium 2013 20th Zittau Fuzzy Colloquium, 183–189.
Firsov, S. N., Reznikov, O. V. (2014). Hardware–software complex experimental development management processes, diagnosing failures and parry of small spacecraft. Journal of Devices and Systems. Management, monitoring, diagnostics, 6, 60–69.
Ovchinnikov, M. (2012).Proceedings of the meeting "Motion control of small satellites". Moskov, Keldysh RAS, 32.
Ovchinnikov, M. (2011) Proceedings of the 3rd meeting of the "Motion control of small satellites". Moskov, Keldysh RAS, 26.
Lyubimov, V. V. (2009). On peculiarities in the perturbed rotational motion of a satellite with a strong magnet on board. Proceedings of the higher educational institutions. Aviation equipment, 2, 29–31.
Meschanov, A. S. (2008). The method of equivalent transformations to control observation satellite inertial actuators with uncertainty. Proceedings of the higher educational institutions. Aeronautics, 3, 258–268.
Meschanov, A. S. (2009). Precision control observation satellite with low energy costs. Proceedings of the higher education institutions. Aeronautics, 1, 17–23.
Afanasiev, V. A. (2013). Manage reversals spacecraft for the appointed time using rocket engines. Proceedings of the higher education institutions. Aeronautics 1, 21–26.
Firsov, S. N. (2013) Ensuring functional stability parameter meter motion satellite systems stabilization and orientation. Journal of Radіoelektronіka, іnformatika, upravlіnnya, 1 (28), 144–150.
Bandurv, І.,M., Fіrsov, S. M., Locale, S. V. (2014). Patent 87065 Ukraine, MKІ B 64 G 1/24. A method of damping the angular velocity spacecraft. National Aerospace University. ME Zhukovsky "hai". № 87 065; Appl. 6/10/13; Publish. 01.27.14, Bull number 2, 3.
Firsov, S. N. (2014). Methodology for ensuring the stability of functional satellite systems. LAP LAMBERT Academic Publishing, 208.
Luchenko, O. A., Taran, A. N., Firsov, S. N. (2011). Determination of parameters of the installation of motor flywheel system orientation and stabilization of asymmetric malogaba–ritnogo spacecraft. Journal of Aerospace and Technology, 1 (78), 63–68.
Firsov, S. N. (2014). Formation resistant to failure of engine blocks flywheels satellite systems stabilization and orientation. Journal of Theory and Control Systems, 4 (83), 83–104.
Postnikov, V. N., Taran, A. N., Firsov, S. N. (2011). Criteria for evaluating the properties of redundant systems flywheel. Journal of Radіoelektronіka, іnforma–teak upravlіnnya, 4, 87–82.
Taran, A. N., Firsov, S. N., Bychkova, I. V. (2011). The concept of survivability of satellite attitude control systems and stabilization. Journal of Information Processing Systems, 8 (98), 127–129.
Firsov, S. N. (2012). Analytical method for determining the parameters of the control system of the spacecraft orientation. Journal of Aerospace and Technology, 4 (91), 55–59.
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