Adaptation of Pendulum Correction of an Airborne Strapdown Vertical Gyroscope to Aircraft Flight Conditions
https://doi.org/10.17285/0869-7035.2016.24.4.025-034
Abstract
An algorithm of a vertical gyroscope with MEMS sensors used to detect pitch and roll angles of aircraft is considered. It is suggested to integrate inertial sensors with an air data system. A flight simulator is used to optimize the algorithm coefficients.
About the Authors
B. O. Kachanov
Uspensky Avionica Moscow Research and Production Complex JSC
Russian Federation
Russian Federation
D. V. Grishin
Moscow Aviation Institute (National Research University)
Russian Federation
Russian Federation
S. K. Akhmedova
Uspensky Avionica Moscow Research and Production Complex JSC
Russian Federation
Russian Federation
N. A. Tuktarev
Uspensky Avionica Moscow Research and Production Complex JSC
Russian Federation
Russian Federation
V. S. Kulabukhov
Uspensky Avionica Moscow Research and Production Complex JSC
Russian Federation
Russian Federation
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Review
For citations:
Kachanov B.O., Grishin D.V., Akhmedova S.K., Tuktarev N.A., Kulabukhov V.S. Adaptation of Pendulum Correction of an Airborne Strapdown Vertical Gyroscope to Aircraft Flight Conditions. Giroskopiya i Navigatsiya. 2016;24(4):25-34. (In Russ.) https://doi.org/10.17285/0869-7035.2016.24.4.025-034
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