Ensuring maximum stability of Earth remote sensing conditions without the orbit correction
Heading:
| 1Ivanova, VI, 1Sheptun, AD 1Yangel Yuzhnoye State Design Office, Dnipropetrovsk, Ukraine |
| Space Sci.&Technol. 2016, 22 ;(2):38-47 |
| https://doi.org/10.15407/knit2016.02.038 |
| Publication Language: Russian |
Abstract: We investigated factors affecting the deviation of the local solar time of an ascending node of sun-synchronous orbits. We derived the relations for calculation of amendment to the basic inclination, which minimizes this deviation in the range of operation of the spacecraft in orbit. The use of the amendment will minimize or eliminate the orbit corrections. The theoretical results are confirmed by observations of the actual flights of the “Ocean-O” and “Egyptsat-1” spacecrafts developed by the Yangel Yuzhnoye State Design Bureau.
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2. Ivanova V. I., Sheptun A. D. Minimization of deviation from local sun time of sun synchronous orbit ascending node considering injection accuracy. Aerospace technic and technology, No. 2(119), 52—56 (2015) [in Russian].
3. Mishin V. P. Space Flight Mechanics, 407 p. (Mashinostroenie, Moscow, 1989) [in Russian].
4. Chernov A. A., Chernjavskij G. M. The orbits of the Earth remote sensing satellites, 200 p. (Radio i svjaz', Moscow, 2004) [in Russian].
5. Chernjavskij G. M., Bartenev V. A., Malyshev V. A. Control of stationary satellite’s orbit, 143 p. (Mashinostroenie, Moscow, 1984) [in Russian].
6. Sheptun A. D., Ivanova V. I., Mashtak I. V. The application of the theorem of change of angular momentum to the problem of the secular movement of the plane of the orbit solar synchronous orbit Space technology. Missiles, No.1, 29—36 (2013) [in Russian].
7. Elyasberg P. E. Introduction to the theory of flight. 540 p. (Nauka, Moscow, 1965) [in Russian].
8. Vallado D. A. Fundamentals of Astrodynamics and Applications. Vol. 2 (McGraw-Hill, New York, 2001).