Test complex for the onboard navigation system of an airport ground vehicle

Антонов, Д. А.; Veremeenko, K. K.; Zharkov, M. V.; Zimin, R. Yu.; Kuznetsov, I. M.; Pron’kin, A. N.

doi:10.1134/s106423071604002x

Cited by 8 publications

(2 citation statements)

References 1 publication

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“…The car test was carried out with the use of an inertial measurement unit Litef LCI [13], based on fiber optic gyroscopes, and NovAtel OEMV GNSS receivers included in the MAI Navigation System Car Testbed installed inside a car roof rack [14] (Figure 2). The car test experimental setup is shown on Figure 3.…”

Section: Car Testmentioning

confidence: 99%

Experimental Results of Attitude Determination Functional Algorithms Implementation in Strapdown Inertial Navigation System

Zharkov

Veremeenko

Kuznetsov

et al. 2022

Sensors

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Strapdown inertial navigation system (SINS) software developers are usually mainly focused on the attitude determination algorithm design and characteristics. Such an algorithm can be based on different mathematical apparatus. An approach to the derivation of attitude determination algorithm equations in strapdown inertial navigation system is proposed. This algorithm is based on direct heading, pitch, and roll calculation. The qualitative differences between the proposed algorithm and the one using a transformation matrix are noted. The main objective of the paper is direct attitude angles calculation algorithm application possibilities analysis in real SINS operating conditions. The analysis is based on a comparison of the proposed algorithm with another frequently used attitude determination algorithm based on the transformation matrix. Attitude determination algorithms performance investigation results based on car and helicopter experimental tests are presented.

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Section: Car Testmentioning

confidence: 99%

Experimental Results of Attitude Determination Functional Algorithms Implementation in Strapdown Inertial Navigation System

Zharkov

Veremeenko

Kuznetsov

et al. 2022

Sensors

View full text Add to dashboard Cite

show abstract

“…For example, in (Antonov et al, 2015) and (Antonov et al, 2016), it is proposed to install additional devices such as a satellite navigation receiver, a micromechanical inertial navigation system, an odometer and/or a relative velocity sensor on board mobile objects. The authors believe that the coordinated determination's achieved accuracy will allow to apply such an improved system even for driving unmanned vehicles.…”

Section: Introductionmentioning

confidence: 99%

Time and Space Discretization in the Digital Twin of the Airport Transport Network

Saifutdinov

Tolujevs

2021

Transport and Telecommunication Journal

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The paper describes the concept of a Digital Twin (DT) creation, which could be used as part of a centralized ground traffic control system in the airport’s apron area. The work is focused on the automatic control systems expected in the future, which will completely replace the ground traffic controllers that solve the centralized control’s tasks in our days. It is assumed that the developed DT can be used both at the stage of training the control system and at the stage of its use. A special feature of the proposed DT concept is the clearly formulated principles of the observed process’ time discretization and the space in which the movement of ground vehicles and aircraft occurs. The experimental verification of the developed concept was carried out using a special simulation model designed to generate data streams on the airport’s transport network’s traffic participants’ location.

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Attitude sensors relative angular misalignment estimation in integrated navigation systems

Kuznetsov

Veremeenko

Zharkov

et al. 2022

MATEC Web of Conferences

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When using modern navigation systems as part of an on-board system, the navigation task can be solved in several ways: using positional, velocity and angular corrections, and systems using measurements of various physical nature—radio, such as short-range and long-range navigation radio systems, GLONASS/GPS satellite global navigation systems, optical—celestial navigation systems—can operate as correctors. The best performance of INS and its sensors (gyroscopes and accelerometers) errors estimation can be obtained when all types of correction are implemented simultaneously. At the same time, it is particularly difficult to implement correction according to attitude parameters due to the fact that the measuring axes of the INS and correctors may not match on board of moving objects. Such a mismatch is commonly called relative angular misalignment. The paper considers a possible approach to the attitude sensors relative angular misalignment estimation in integrated navigation systems (NS), carried out in motion when the NS is in operating mode.

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Test complex for the onboard navigation system of an airport ground vehicle

Cited by 8 publications

References 1 publication

Experimental Results of Attitude Determination Functional Algorithms Implementation in Strapdown Inertial Navigation System

Experimental Results of Attitude Determination Functional Algorithms Implementation in Strapdown Inertial Navigation System

Time and Space Discretization in the Digital Twin of the Airport Transport Network

Attitude sensors relative angular misalignment estimation in integrated navigation systems

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