Keywords: electrically suspended gyroscope (ESG), strapdown stabilized gyrocompass, fiber-optic gyroscope, micromechanical sensors (MEMS)
References
1. Buravlev A.P., Kuzin V.M., Landau B.E., Sumarokov V.V. Beskardannyi elektrostaticheskii giroskop s podvesom na dvoinykh elektrodakh [Strapdown electrostatic gyro suspension on double electrodes]. XXVI Nauchno-Tekhnicheskaya Konferentsiya Pamyati N.N.Ostryakova: Doklady [XXVI Scientific Conference N.N. Ostryakova Memory: Reports]. St. Petersburg, 2008, pp. 17–18.
2. Emel'yantsev G.I., Landau B.E., Levin S.L., Gurevich S.S., Romanenko S.G. Integrated attitude reference and navigation system for orbital spacecraft. Gyroscopy and Navigation, vol. 2, no. 3, 2011, pp. 146–151. doi: 10.1134/S2075108711030035
3. Landau B.E., Belash A.A., Gurevich S.S., Emeliantsev G.I., Levin S.L., Romanenko S.G. Beskardannaya inertsial'naya sistema orientatsii na elektrostaticheskikh giroskopakh dlya orbital'nogo kosmicheskogo apparata [Cardan-less inertial orientation system with electrostatic gyroscopes for orbital spaceship]. Izv. vuzov. Priborostroenie, 2011, vol. 54, no. 6, pp. 66–74.
4. Emeliantsev G.I., Landau B.E., Levin S.L., Gurevich S.S., Romanenko S.G. Osobennosti postroeniya integrirovannoi sistemy orientatsii i navigatsii dlya orbital'nogo kosmicheskogo apparata [Specifics of an Integrated Attitude Reference and Navigation System for Orbital Spacecraft]. Giroskopiya i Navigatsiya, 2011, no. 1, pp. 17–25.
5. Nikishin V.B., Sinev A.I., Plotnikov P.K., Naumov S.G. Povyshenie tochnosti podzemnoi navigatsii na osnove integratsii BINS, odometrov i priemnikov GPS/GLONASS [Increasing the accuracy of underground navigation based on the integration of SINS, odometers and receivers of GPS / GLONASS]. Materialy XVII Mezhdunarodnoi Konferentsii po Integrirovannym Navigatsionnym Sistemam [Proc. XVII Int. Conf. on Integrated Navigation Systems]. St. Petersburg, 2010, pp. 169–174.
6. Emelyantsev G.I., Lochekhin A.V. O pogreshnostyakh beskardannogo girogorizontkompasa na elektrostaticheskom giroskope i mikromekhanicheskikh datchikakh [Errors of cardan-less gyro-horizon-compas with electrostatic gyroscope and micromechanical sensors]. Izv. vuzov. Priborostroenie, 2010, vol. 53, no. 10, pp. 42–48.
7. Blazhnov B.A., Volynskii D.V., Emel'yantsev G.I., Nesenyuk L.P., Stepanov A.P. Integrirovannaya inertsial'no-sputnikovaya sistema orientatsii i navigatsii s mikromekhanicheskim inertsial'nym modulem. Rezul'taty ispytanii na avtomobile [Integrated inertial-satellite attitude control system and micromechanical inertial navigation unit. Test results on the vehicle]. Giroskopiya i Navigatsiya, 2008, no. 4 (63), p. 77.
8. BlazhnovB.A., EmeliantsevG.I., KoshaevD.A., SemenovI.V.,StepanovA.P.,ZhilinskiiV.M.,KorotkovA.N.,TimofeevE.A.,Tsekhanovich G.S. Integratedtightlycoupledinertialsatelliteorientationandnavigationsystem.Gyroscopy and Navigation, 2010, vol. 1, no. 1, pp. 10–18. doi: 10.1134/S2075108710010037
9. Volynskii D.V., Odintsov A.A., Dranitsyna E.V., Untilov A.A. Calibration of fiber-optic gyros within strapdown inertial measurement units. Gyroscopy and Navigation, 2012, vol. 3, no. 3, pp. 194–200. doi: 10.1134/S2075108712030108
10.Gusinsky V.Z., Lesyuchevsky V.M., Litmanovich Yu.A. Calibration and alignment of inertial navigation systems with multivariate error state vector. Proc. 4th St. Petersburg International Conference on Integrated Systems. St. Petersburg, 1997. P. 371–378.
11.Anuchin O.N., Emel'yantsev G.I. Integrirovannye Sistemy Orientatsii i Navigatsii dlya Morskikh Podvizhnykh Ob"ektov [Integrated System for Orientation and Navigation of Maritime Objects]. St. Petersburg, TsNII Elektropribor Publ., 2003, 390 p.
12.Landau B.E., Gurevich S.S., Emel'yantsev G.I., Levin S.L., Romanenko S.G., Odintsov B.V. Rezul'taty kalibrovki elektrostaticheskikh giroskopov v beskardannoi inertsial'noi sisteme orientatsii [The calibration results in electrostatic gyro strapdown inertial orientation system]. Materialy XV Mezhdunarodnoi Konferentsii po Integrirovannym Navigatsionnym Sistemam [Proc. XVII Int. Conf. on Integrated Navigation Systems]. St. Petersburg, 2008, pp. 122–129.
13.Landau B.E., Gurevich S.S., Emeliantcev G.I., Levin S.L., Romanenko S.G. Calibrating the error of a strapdown ESG-based attitude reference system under conditions of orbital flight. Gyroscopy and Navigation, 2010, vol. 1, no. 3, pp. 176–182. doi: 10.1134/S2075108710030041
14.Landau B.E., Levin S.L., Gurevich S.G., Emel'yantsev G.I., Zavgorodnii V.I., Romanenko S.G., Odintsov B.V. Nazemnaya otrabotka metodiki poletnoi kalibrovki BISO na ESG dlya orbital'nykh kosmicheskikh apparatov s proizvol'noi orientatsiei [Ground testing methodology flight calibration GIACS on ESG for orbital spacecraft with an arbitrary orientation]. Materialy XIX Sankt-Peterburgskoi Mezhdunarodnoi Konferentsii po Integrirovannym Navigatsionnym Sistemam [Proc. XIX Int. Conf. on Integrated Navigation Systems]. St. Petersburg, 2012, pp. 127–135.
15.Emeliantsev G.I., Landau B.E., Levin S.L., Romanenko S.G. Refining the drift model of a gimballess inertial attitude control system based on electrostatic gyros: methods of calibration on a ground-based test bench and on board an orbiting space vehicle. Gyroscopy and Navigation, 2010, vol. 1, no. 2, pp. 134–140. doi: 10.1134/S2075108710020082
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