Astroinertial integrated navigation system

1Degtyarev, AV, 1Makarov, AL, 1Davydenko, SA, 1Tykhonov, VL, 2Laush, AG
1Yangel Yuzhnoye State Design Office, Dnipropetrovsk, Ukraine
2Co. Ltd. «Navis-Ukraine», Smila, Ukraine
Space Sci.&Technol. 2016, 22 ;(2):29-37
Section: Spacecraft Dynamics and Control
Publication Language: Russian
We discuss the possibility of interconnecting a variety of navigational systems and propose the astroinertial integrated navigation system, which can be used as a part of the control systems of various carrier rockets.
Keywords: Gimballess Inertial Navigation System (GINS), Satellite Navigation System User Equipment (SN SUE), Sensitive elements on the basis of Microelectromechanical Systems (MEMS)
1. Poshehonov V. G., Sharygin B. L., Mironov K. V. Unified system of inertial navigation and stabilization of "Ladoga-M'.Marine electronics, No. 1 (4), P. 26—30 (2003) [in Russian].
2. Reznichenko V. I., Lapshina V. I. Organization of interaction of satellite and autonomous facilities of the marine objects. (GNINGI RF, SPb, 2004) [in Russian].
3. Pervan B. S., Pullen S. P., Christie J. R. A Multiple Hypothesis Approach to Satellite Navigation Integrity. Navigation, 45 (1), 61—84 (1998).
4. Windl J., et al. Flight and Landing Trials with combined DGPS/DGLONASS/INS System for Dynamic Maneuvers and Precision Landings. ION GPS-98 Proc. (Nashwill, 1998).