A backup orientation system based on inverse problems technique

• Autorzy: Nenarokomov Aleksey V. , Chebakov Evgeny V. , Krainova Irina V. , Reviznikov Dmitry L. , Morzhukhina Alena V.

Identyfikatory

DOI

10.24423/cames.250

• Języki publikacji: EN

Abstrakty

EN

The correct orientation of the spacecraft during a space flight is one of the main tasks of astronautics,because its orientation affects the correct operation of all subsystems, in particular power supply systems,where the orientation of solar panels is one of the key tasks. From this point of view, the tasks of developingbackup or replacement of orientation systems are becoming relevant. In this paper, an alternative for thedevelopment of an orientation sensor is proposed, which is sensitive to radiation heating from the Sun orother celestial bodies that emit strongly. Thus, the tasks of developing a heat flux sensor responsive tochanges in heat fluxes become relevant. This article is devoted to the analysis of technical capabilitiesto create such a sensor.

Słowa kluczowe

EN

computational method; measurement; instrumentation; radiation; inverse problem; or-bital spacecraft; orientation

PL

metoda obliczeniowa; pomiar; oprzyrządowanie; promieniowanie; problem odwrotny; orbitalny statek kosmiczny; orientacja

• Wydawca: Instytut Podstawowych Problemów Techniki PAN
• Czasopismo: Computer Assisted Methods in Engineering and Science
• Rocznik: 2019
• Tom: Vol. 26, no. 2
• Strony: 79--91
• Opis fizyczny: Bibliogr. 5 poz., rys., wykr.

Twórcy

autor

Nenarokomov Aleksey V.

• Moscow Aviation Institute Volokolamskoe 4, Moscow, 125993, Russia

autor

Chebakov Evgeny V.

• Moscow Aviation Institute Volokolamskoe 4, Moscow, 125993, Russia

autor

Krainova Irina V.

• Moscow Aviation Institute Volokolamskoe 4, Moscow, 125993, Russia

autor

Reviznikov Dmitry L.

• Moscow Aviation Institute Volokolamskoe 4, Moscow, 125993, Russia
• Dorodnicyn Computing Centre Vavilov 44 (b. 2), Moscow, 119333, Russia

autor

Morzhukhina Alena V.

• Moscow Aviation Institute Volokolamskoe 4, Moscow, 125993, Russia

Bibliografia

• [1] O.M. Alifanov. Inverse Heat Transfer Problems. Berlin: Springer-Verlag, 1994.
• [2] I.V. Gritsevich (Krainova), A.V. Nenarokomov. Determining the external thermal action on the surface of an orbital spacecraft. In: Thermal Processes in Technology[in Russian], Nauka i Tekhnologii, Moscow, Vol. 5,No. 10, pp. 445-457, 2013.
• [3] L.V. Kozlov, M.D. Nusinov, A.I. Akishin, V.M. Zaletaev, V.V. Kozelkin. Modeling of spacecraft thermal regimes and its environment. Moscow: Mashinostroenie, 1971 [in Russian].
• [4] N.P. Semena. Determination of spacecraft orientation by the temperature field analysis of its outer surface. Thermophysics and Aeromechanics,16(1): 129–140, 2009.
• [5] A.N. Tikhonov, V.Y. Arsenin. Solution of Ill-Posed Problems. New York, Toronto, London, Sydney: John Wiley and Sons, 1977.