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Том 10, № 2 (2019)
- Год: 2019
- Статей: 7
- URL: https://bakhtiniada.ru/2075-1087/issue/view/12723
Article
Synthesis of Calibration Programs for an Accelerometer Unit of Strapdown INS: An Invariant Approach
Аннотация
The paper considers the synthesis of the calibration programs for an accelerometer unit of strapdown inertial navigation systems (INS) and estimation of the accuracy characteristics they provide. The study is carried out in the framework of an invariant approach. The synthesis criteria and additional requirements that the calibration programs must meet are formulated. A comparative analysis of accuracy characteristics of different calibration programs has been performed.
70-76
Initial Alignment of SINS Measuring Unit and Estimation of Its Errors Using Satellite Phase Measurements
Аннотация
The paper addresses the problem of initial alignment and periodical estimation of gyro drifts and accelerometer errors in a strapdown inertial navigation system (SINS) on fiber-optic gyros (FOG) of navigation grade onboard a marine vehicle, using satellite phase measurements from multi-antenna equipment. The problem is solved through constructing a tightly-coupled INS/GNSS system which comprises an inertial measuring unit (IMU) of SINS, and a multi-antenna satellite module. The satellite module has two antenna baselines and employs receivers with a common reference oscillator. Based on the SINS data, the ambiguity of phase measurements is excluded, and false measurements are sorted out. The results of joint processing of the bench test data for the navigation grade FOG-based IMU (designed by Concern CSRI Elektropribor, JSC) and a virtual simulated satellite module are presented. The data processing was carried out using the algorithms of integrated system construction in MATLAB (Simulink) package.
62-69
Selected Features of Autonomous Underwater Robot Dynamics under Near-Bottom Equidistant Motion Control
Аннотация
Search and survey missions of an autonomous underwater robot are usually associated with motion along equidistant trajectories near the bottom. The most difficult problem here is to control motion in a vertical plane in presence of obstacles in the bottom relief along the motion route. When the obstacles are detected using a multi-channel front-viewing echolocation system, equidistant motion of the vehicle is provided with tracking of the bottom relief profile. The dynamic model of motion with specific requirements for the structure and control parameters is studied. Comparative analysis of the dynamic properties of control system depending on the design and functional features of the actuating elements and the range-measuring echolocation system is presented.
90-98
Analytical Algorithm for Attitude and Heading Estimation Aided by Maneuver Classification
Аннотация
This paper presents a modified adaptive analytical algorithm for attitude and heading estimation. The analytical algorithm is based on the fusion of IMU, magnetometers and the velocity data from GPS. The kinematic Euler angles are first calculated based on the output of the rate gyros, then the calculated angle errors are compensated using the output of each of the accelerometers, magnetometers, and the velocity taken from a GPS receiver, without the need to model the systematic and random errors of the used sensors; Kalman filter is not used. The algorithm will be adaptive based on the maneuver classification, the filters’ parameters will be tuned depending on the maneuver intensity: No, Low, or High maneuver. The main contribution of this paper is to build an attitude and heading estimation algorithm (analytical algorithm) without using Kalman filter; this algorithm will be made adaptive based on the maneuver classification algorithm which was developed using logistic regression technique based on IMU output. Computer simulation with simulated and real flight data showed that the adaptive analytical algorithm has acceptable results compared to EKF.
77-89
Satellite Navigation of Lunar Orbiting Spacecraft and Objects on the Lunar Surface
Аннотация
A concept of a global lunar navigation satellite system (GLNSS) based on the existing navigation infrastructure of the GLONASS is proposed. It is supposed to be implemented through the creation of a constellation of navigation satellites in the Earth orbit to serve the needs of both lunar spacecraft and objects on the lunar surface. Two variants for the deployment of the orbital constellation are considered. The navigation solution in the vicinity of the Moon was simulated using signals from the proposed GLNSS. The accuracy of the GLNSS navigation solutions has been estimated for all types of users.
54-61
GPS Based Navigation Systems in Difficult Environments
Аннотация
Position, velocity, and timing (PVT) signals from the Global Positioning System (GPS) are used throughout the world but the availability and reliability of these signals in all environments has become a subject of concern for both civilian and military applications. This presentation summarizes recent advances in navigation sensor technology, including GPS, inertial, and other navigation aids that address these concerns. Also addressed are developments in sensor integration technology with several examples described, including the Bluefin-21 system mechanization.
41-53
Calibration of Integral Magnetometer Linear Model Coefficients Using Simultaneous Measurements of a Three-Axis Gyro
Аннотация
The paper considers a problem of calibration of a three-axis magnetometer integrated in a complex electronic device. Known methods of calibration based on the ellipsoid approximation of the geometric locus of magnetometer measurements provide only partial calibration and determine only the symmetrical part of the magnetic permeability matrix. The orthogonal part of the matrix remains undetermined. The proposed algorithm makes it possible to find the full matrix of magnetic permeability with the use of device rotation and additional measurements made by a three-axis gyro.
99-110