Zobrazeno 1 - 10
of 26
pro vyhledávání: '"I M, Kuznetsov"'
Publikováno v:
Cybernetics and Systems Analysis. 58:691-701
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
Autor:
Valentina Gritsenko, S V Ryzhova, Vsevolod Konstantinov, O S Pavlova, E A Аlexandrova, V A Shorokhova, I M Kuznetsov, O E Khukhlaev
Publikováno v:
Культурно-историческая психология, Vol 15, Iss 3, Pp 71-82 (2019)
The current research studies the problems connected with interrelation between religiosity and intergroup hostility (or prejudice). We hypothesized and verified the connection between identification with religious group and ethno-national attitudes.
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:
L N, Bisenkov, B V, Gaĭdar, Iu N, Shanin, V E, Parfenov, S A, Shalaev, O V, Orzheshkovskiĭ, I M, Kuznetsov, R Ia, Guniat
Publikováno v:
Vestnik khirurgii imeni I. I. Grekova. 165(6)
The work presents an experience with the diagnosing of synchronous tumors of double localization in 256 patients. Operations were performed on 146 of them. Single-stage operations were made in 55 cases. When performing single-stage operations, 20 pat
Publikováno v:
Voprosy onkologii. 52(4)
Incidence of lung cancer associated with secondary paracancerous changes is known to range 13.7-30%. Since they reveal such clinical symptoms as pneumonia or empyema, most out-patients with complicated cancers are referred to general wards. Inflammat