Abstract
Brief description of a model of a vector gravimetric system using astronomic and satellite positioning data is given in terms of the inertial navigation method, and the results of numerical investigation of the system are reported.
References
A. Yu. Ishlinskii, Classical Mechanics and Inertial Forces (Nauka, Moscow, 1987) [in Russian].
V. D. Andreev, Theory of Inertial Navigation: Aided Systems (Nauka, Moscow, 1967; Israel Program for Scientific, Jerusalem, 1969).
Gravity Surveying: A Geophysicist’s Handbook, Ed. by E. A. Mudretsova and K. E. Veselov (Nedra, Moscow, 1981) [in Russian].
A. S. Devyatisil’nyi, Zh. Tekh. Fiz. 79(12), 103 (2009) [Tech. Phys. 54, 1825 (2009)].
A. S. Devyatisil’nyi and N. A. Prudkoglyad, Aviakosm. Priborostr., No. 11, 39 (2007).
R. E. Kalman P. L. Falb, and M. A. Arbib, Topics in Mathematical System Theory (McGraw-Hill, New York, 1969; Mir, Moscow, 1971).
Yu. S. Osipov and A. V. Kryazhimskii, Vestn. Ross. Akad. Nauk 76, 615 (2006).
A. S. Devyatisil’nyi and I. B. Kryzhko, Kosm. Issled. 35, 99 (1997).
Author information
Authors and Affiliations
Corresponding author
Additional information
Original Russian Text © A.S. Devyatisil’nyi, 2012, published in Zhurnal Tekhnicheskoi Fiziki, 2012, Vol. 82, No. 1, pp. 143–146.
Rights and permissions
About this article
Cite this article
Devyatisil’nyi, A.S. Model of a correctable inertial navigation system capable of determining the Earth’s gravitational field strength. Tech. Phys. 57, 141–144 (2012). https://doi.org/10.1134/S1063784212010069
Received:
Accepted:
Published:
Issue Date:
DOI: https://doi.org/10.1134/S1063784212010069