Zobrazeno 1 - 10
of 10
pro vyhledávání: '"K. K. Veremeenko"'
Publikováno v:
Russian Aeronautics. 63:618-626
The way of small aircraft strapdown inertial navigation system transfer alignment based on information from the carrier navigation system is considered. Optimal Kalman filter was selected as the main mathematical technique for the proposed method imp
Autor:
I. M. Kuznetsov, R. Yu. Zimin, A. N. Pron'kin, M. V. Zharkov, Dmitry Antonov, K. K. Veremeenko
Publikováno v:
Journal of Computer and Systems Sciences International. 59:261-275
The structure and software of a complex navigation system for an unmanned apparatus are presented. It includes a platformless inertial navigation system, receivers of the satellite navigation system, and a computer vision system. An approach to the c
Publikováno v:
Gyroscopy and Navigation. 9:277-286
Integration of a multiantenna GNSS receiver and inertial sensors (gyroscopes) is proposed to determine attitude parameters using GNSS phase measurements, containing integer ambiguity, and measurements of the absolute rotation rate of a moving vehicle
Publikováno v:
Journal of Physics: Conference Series. 1925:012052
The article presents the attitude determination algorithm for multi-antenna global navigation satellite and inertial integrated navigation system operating under information and measurement insufficiency conditions. The information and measurement in
Publikováno v:
Journal of Physics: Conference Series. 1925:012025
The main unmanned aerial vehicles launched from a carrier aircraft onboard navigation system, usually, is a strapdown inertial navigation system. The paper considers the influence of the time synchronization error in the strapdown inertial navigation
Publikováno v:
IOP Conference Series: Materials Science and Engineering. 927:012073
Attitude determination system is one of the most important system to control the moving object of any type. GNSS attitude determination systems have been actively developed in the last decade. Such systems have obvious drawbacks associated with the n
Autor:
K K Veremeenko, A A Krylov
Publikováno v:
IOP Conference Series: Materials Science and Engineering. 868:012037
This paper is about comparison of two methods of calibration – calibration method for inertial measurement unit with gyroscope and accelerometer direct information outputs and calibration method for strapdown inertial navigation system with coordin
Publikováno v:
2017 24th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS).
A fault-tolerant airport vehicle integrated navigation system as a structural part of Advanced Surface Movement Guidance and Control System (A-SMGCS) is presented in the report. The structure of airport vehicle navigation system algorithms, algorithm
Autor:
K. K. Veremeenko, V. M. Savel'Ev
Publikováno v:
Journal of Computer and Systems Sciences International. 52:106-116
The alignment system of a strapdown inertial navigation system for an unmanned aerial vehicle installed on a carrier aircraft is studied. The aim is to develop alignment techniques for the strapdown inertial navigation system that improve the accurac
Publikováno v:
Scopus-Elsevier
Strap-down inertial and satellite system BISNS-1T developed by these authors from the Moscow Aviation Institute and JSC “Transas-Telematics” at the request of the Joint-Stock Company “Transas-Aviation” is presented. The main objective of this
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