Deployment of long-measured flexible structure in orbit

• Autorzy: Zakrzhevsky A. E.
• Konferencja: Symposium “Vibrations In Physical Systems” (26 ; 04-08.05.2014 ; Będlewo koło Poznania ; Polska)
• Języki publikacji: EN

Abstrakty

EN

Dynamics of the spacecraft with giro-gravitational system of stabilisation, in which the pantograph design deployed in an orbit and containing on the end the concentrated mass is used as the gravitational stabilizer and the carrier of solar batteries, is investigated. The analysis of the obtained information is carried out and graphs that illustrate behaviour of characteristic variables are discussed.

Słowa kluczowe

EN

spacecraft; pantograph structure; deployment

PL

statek kosmiczny; struktura pantografu; wdrażanie

• Wydawca: Poznan University of Technology. Institute of Applied Mechanics
• Czasopismo: Vibrations in Physical Systems
• Rocznik: 2014
• Tom: Vol. 26
• Strony: 335--342
• Opis fizyczny: Bibliogr. 7 poz., rys., wykr.

Twórcy

autor

Zakrzhevsky A. E.

• S. P. Timoshenko Institute of Mechanics NAS of Ukraine, 3, Petra Nesterova Street, Kiev, Ukraine, 03057

Bibliografia

• 1. V. Dranovskii, V. Khoroshylov, A. Zakrzhevskii, Spacecraft dynamics with regard to elastic gravitational stabilizer deployment, Acta Astronautica, 64 (2009) 501-513.
• 2. V. Khoroshilov, A. Kovalenko, A. Zakrzhevsky, Dynamics of deployment of elastic pantograph designs on space vehicle. XXII Symposium - Vibrations in physical systems – Poznań-Będlewo, (2006) 167-172.
• 3. http://www.vibsys.strefa.pl/journal/2006-22/167.pdf
• 4. V. V.Beletsky, Motion of an Artificial Satellite about its Center of Mass, Israel Program for Scientific Translations, Jerusalem, 1966.
• 5. J. Awrejcewicz, Classical Mechanics. Dynamics, Springer-Verlag, New York, 2012.
• 6. A. I. Lurie, Analytical mechanics, Springer, 2002.
• 7. A. E. Zakrzhevskii, Slewing of Flexible Spacecraft with Minimal Relative Flexible Acceleration, J. of Guidance, Control, and Dynamics, 31 (2008) 563- 570.