Abstract
The errors of an autonomous platformless inertial navigation system (INS) with fiber-optic gyros (FOG), the inertial measurement unit (IMU) of which is mounted in a two-axis gimbal suspension, are analyzed. The quality criteria and the kinematic scheme of the gimbal are considered. The optimal law of IMU rotation from the standpoint of the selected minimum criterion has been calculated. Simulation was carried out to study the effects of different errors of the IMU sensors on the INS accuracy. The results obtained are confirmed by the development tests of a FOG-based INS designed by Concern CSRI Elektropribor.
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Department of Defense, Developing Science & Technologies List, Section 16: Positioning, Navigation and Time Technology. Office of the Under Secretary of Defense, Acquisition, Technology and Logistics, Washington, D.C., January 2006.
Barbour, N. and Schmidt, G., Inertial Sensor Technology Trends, IEEE Sensors Journal, vol. 1, no. 4, December 2001, pp. 332–339.
Paturel, Y., Rumoroso, V., Chapelon, A., and Honthaas, J.Y., MARINS, the first FOG navigation system for submarine, Symposium Gyro Technology, 2006.
Walsh, Ed., Navy and industry investigate new superaccurate optical gyros for possible use on ballistic missile submarines, Military & Aerospace Electronics, 2001.
NATO STANAG 4278: Method of expressing navigation accuracies, Brusel-2003.
Svoboda, P., Luzica, S., and Grecman, P., Mode-s positional data error analysis from the point of view of air traffic control, Annals of the University of Craiova, Electrical Engineeiring series, no. 30, 2006, pp. 335–339.
Levinson, E. and Majure R., MARLIN–Next generation marine inertial navigator. Symposium Gyro Technology, Stuttgart, 22–23 Sept., 1987.
Peshekhonov, V.G., Gyroscopic Navigation Systems: Current Status and Prospects, Gyroscopy and Navigation, 2011, vol. 2, no.3, pp. 111–118.
www.sperrymarine.com
www.northropegrumman.com
Guo Wei, Xingwu Long, and Xudong Yu, Research on high precision rotating inertial navigation system with ring laser gyroscope, 22 nd Saint Petersburg Int. Conf. on Integrated Navigation Systems, May, 2015.
Fei Yu and Qian Sun, Angular rate optimal design for the rotary strapdown inertial navigation system, Sensors 2014, 14 (4), pp. 7156–7180.
Zhenguo Yuan and Lin Zhao, Error analysis of rotary SINS sensor, Sensors & Transducers, vol. 156, no. 9, September 2013, pp. 35–39.
www.elektropribor.spb.ru
Gyro indexing compensation method and system; US Patent 8566055 B1, 2013.
Ringlein, M.J., Barnett, N.J., and May, M.B., Next generation strategic submarine navigator Marvin B., AIAA 2000, http://www.researchgate.net
Vaisgant, I. B., Choosing the rate of the INS platform forced rotation, Giroskopiya i Navigatsiya, 1999, no. 4, pp. 116–120.
Lefèvre, H.C., The fiber-optic gyroscope: Achievement and perspective, 19 th Saint Petersburg Int. Conf. on Integrated Navigation Systems, 2012, pp. 122–126.
Slyusar’, V.M., On the effect of instrumental factors on the strapdown INS angular rate drift, Giroskopiya i Navigatsiya, 2009, no.4, pp. 47–61.
Emel’yantsev, G.I., Litmanovich, Yu.A., and Moshkin, N.N., On increasing information autonomy of strapdown INS for marine application, Giroskopiya i Navigatsiya, 2014, no. 3, pp. 15–28.
Zel’dovich, S.M. et al., Avtokompensatsiya instrumental’nykh pogreshnostei (Autocompensation of Instrumental Errors, Leningrad: Sudostroenie, 1976.
Rivkin, S.S. Teoriya giroskopicheskikh ustroistv (Theory of gyroscopic devices), vol. 2, Leningrad: Sudostroenie, 1964.
Luk’yanov, D.P., Mochalov, A.V., Odintsov, A.A., Vaisgant, I.B., Inertsial’nye Navigatsionnye Sistemy Morskikh Ob”ektov (Inertial Navigation Systems of Marine Vehicles, Leningrad: Sudostroenie, 1989.
Ishlinskii, A.Yu., Mekhanika giroskopicheskikh sistem (Mechanics of Gyroscopic Systems), ÀN SSSR, 1963.
Anuchin, O.N. and Emel’yantsev, G.I., Integrirovannye sistemy orientatsii i navigatsii dlya morskikh podvizhnukh ob”ektov (Integrated Navigation and Orientation Systems for Marine Vehicles), St. Petersburg: CSRI Elektropribor, 2003.
Karakashev, V.A., Avtonomnye inertsial’nye navigatsionnye sistemy: uchebnoe posobie (Autonomous Inertial Navigation Systems), Leningrad: LITMO, 1983.
www.sagem.com
Stepanov, A.P., Ignat’ev, S.V., and Vinokurov, I.Yu. et al., Determining the optimum law for control of the rotation drive on the basis of minimization of INS errors, Materialy 4 Vserossiiskoi mul’tikonferentsii po problemam upravleniya MKPU-2011 (Materials of the 4th All-Russian Multi-Conference on the Problems of Control), 2011, vol. 2, Taganrog: TTI YuFU, pp. 316–318.
Blazhnov, B.A., Emel’iantsev, G.I., Koshaev, D.A., Semenov, I.V., Stepanov, A.P., et al. Integrated INS/GPS Orientation and Navigation System Built by a Tightly-Coupled Scheme, XVI Sankt-Peterburgskaya mezhd. konf. po integrirovannym informatsionnym sistemam (XVI Saint-Petersburg Int. Conf. on Integrated Information Systems), St.Petersburg, 25–27 May, 2009, pp. 153–162.
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Published in Giroskopiya i Navigatsiya, 2015, No. 4, pp. 42–54.
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Stepanov, A.P., Emel’yantsev, G.I. & Blazhnov, B.A. On the effectiveness of rotation of the inertial measurement unit of a FOG-based platformless ins for marine applications. Gyroscopy Navig. 7, 128–136 (2016). https://doi.org/10.1134/S2075108716020103
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DOI: https://doi.org/10.1134/S2075108716020103