Abstract
The developed spatial (3D) orbital gyrocompass allows performing all the necessary functions of angular orientation of a spacecraft relative to the orbital coordinate system. In this regard, it is no different from the astronavigation system (ANS), except for the use of different types of external information sensors. In the first case, it is the Earth orientation device; in the second case, it is the star sensor. Each system has its advantages and disadvantages. The advantage of the ANS is higher orientation accuracy. The undeniable advantage of the 3D gyrocompass is the ability to control the orientation of the spacecraft for an extended period without using ballistic data. The sufficiently high functionality of the 3D gyrocompass makes the orientation system built on its basis quite competitive with astronavigation-based orientation systems. Thus, the task of studying the properties and improving the accuracy characteristics of the device becomes relevant.
REFERENCES
Abezyaev, I.N., Gyrocompass for orbital space vehicles, Cosmic Res., 2021, vol. 59, no. 3, pp. 204–211. https://doi.org/10.1134/S0010952521030011
Braison, A.E. and Kortyum, V., Calculation of the local angular position of an orbiting spacecraft, Proc. 3rd Int. Symp. IFAC, Toulouse, France, 1970, vol. 2, pp. 83–89.
Raushenbakh, B.V. and Tokar’, E.N., Upravlenie orientatsiei kosmicheskikh apparatov (Spacecraft Attitude Control), Moscow: Nauka, 1974.
Abezyaev, I.N., RF Patent 2579406, 2014.
Bo Xu, Yang Liu, Wei Shan, et al., Error analysis and compensation of gyrocompass alignment for SINS on moving base, Mathematical Problems in Engineering, 2014, p. 373575. https://doi.org/10.1155/2014/373575
Major, F.G., The mechanical gyrocompass, in Quo Vadis: Evolution of Modern Navigation, New York: Springer, 2014. https://doi.org/10.1007/978-1-4614-8672-5_12
Reid, D.B., Orbital gyrocompass evolution, DGON Intertial Sensors and Systems (ISS), 2016, vol. 20, pp. 149–170. https://doi.org/10.1109/INERTIALSENSORS.2016.7745672
Abezyaev, I.N., Velichko, P.E., and Potselovkin, A.I., Optimization of the method for calibrating orbital gyrocompass errors in flight conditions, Tr. FGUP NPTsAP. Sistemy i pribory upravleniya, 2020, no. 3, pp. 5–14.
Bel’skii, L.N., Vodicheva, L.V., and Parysheva, Yu.V., Strapdown inertial navigation system for launch vehicles: initial alignment accuracy and periodic calibration, in Yubileinaya 15-ya Sankt-Peterburgskaya Mezhdunarodnaya konf. po integrirovannym navigats. sistemam (Anniversary 15th St. Petersburg Int. Conf. on Integrated Navigation Systems), 2018, pp. 250–253.
Boyarchuk, K.A. and Nekhamkin, L.I., Orientation and stabilization system of the Condor-E spacecraft, in Trudy sektsii 22 imeni V.N. Chelomeya 38-kh Akadem. chtenii po kosmonavtike (Proceedings of Section 22 named after V.N. Chelomei of the 38th Academic Readings on Astronautics), 2015, vol. 22, pp. 408–424.
Bordachev, D.A., Volyntsev, A.A., Ilyushin, P.A., et al., Results of ground testing of a precision gyroscopic angular velocity meter of a spacecraft, Giroskopiya i navigatsiya, 2015, no. 4 (91), pp. 106–116. https://doi.org/10.17285/0869-7035.2015.23.4.106-116
Vavilova, N.B., Vasineva, I.A., Golovan, A.A., et al., The calibration problem in inertial navigation, J. Math. Sci., 2021, vol. 253, pp. 818–836.
Vavilova, N.B., Golovan, A.A., and Parusnikov, N.A., Kratkii kurs teorii inertsial’noi navigatsii (A Short Course on the Theory of Inertial Navigation), Moscow: Inst. Probl. Upravl. Ross. Akad. Nauk, 2022.
Golovchenko, A.A. and Golovchenko, L.V., RF Patent 2466068, 2012.
Abezyaev, I.N., Velichko, P.E., Potselovkin, A.I., et al., Development of the algorithm of the spacecraft programmed yaw turns with the use of orbital gyrocompass, AIP Conf. Proc., 2019, vol. 2171, no. 1, p. 060009. https://doi.org/10.1063/1.5133207
Funding
This work was supported by ongoing institutional funding. No additional grants to carry out or direct this particular research were obtained.
Author information
Authors and Affiliations
Corresponding author
Ethics declarations
The author of this work declares that he has no conflicts of interest.
Additional information
Translated by M. Chubarova
Publisher’s Note.
Pleiades Publishing remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.
Rights and permissions
About this article
Cite this article
Abezyaev, I.N. Spatial Orbital Gyrocompass. Questions of Theory and Application. Cosmic Res 62, 99–105 (2024). https://doi.org/10.1134/S0010952523700740
Received:
Revised:
Accepted:
Published:
Issue Date:
DOI: https://doi.org/10.1134/S0010952523700740