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  Subjects -> AERONAUTICS AND SPACE FLIGHT (Total: 124 journals)
Showing 1 - 30 of 30 Journals sorted alphabetically
Acta Astronautica     Hybrid Journal   (Followers: 220)
Advances in Aerospace Engineering     Open Access   (Followers: 74)
Advances in Aerospace Science and Technology     Open Access   (Followers: 14)
Advances in Astronautics Science and Technology     Hybrid Journal   (Followers: 2)
Advances in Space Research     Hybrid Journal   (Followers: 295)
Aeronautical Journal, The     Hybrid Journal   (Followers: 9)
Aerospace     Open Access   (Followers: 64)
Aerospace Medicine and Human Performance     Full-text available via subscription   (Followers: 22)
Aerospace Science and Technology     Hybrid Journal   (Followers: 305)
Aerospace Systems     Hybrid Journal   (Followers: 10)
Aerospace technic and technology     Open Access   (Followers: 7)
Aerotecnica Missili & Spazio : Journal of Aerospace Science, Technologies & Systems     Hybrid Journal   (Followers: 6)
AIAA Journal     Hybrid Journal   (Followers: 1002)
Air Medical Journal     Hybrid Journal   (Followers: 6)
Aircraft Engineering and Aerospace Technology     Hybrid Journal   (Followers: 139)
Artificial Satellites     Open Access   (Followers: 21)
ASTRA Proceedings     Open Access   (Followers: 3)
Astrodynamics     Hybrid Journal   (Followers: 4)
Aviation     Open Access   (Followers: 12)
Aviation in Focus - Journal of Aeronautical Sciences     Open Access   (Followers: 7)
Aviation Psychology and Applied Human Factors     Hybrid Journal   (Followers: 23)
Aviation Week     Full-text available via subscription   (Followers: 411)
Canadian Aeronautics and Space Journal     Full-text available via subscription   (Followers: 31)
CEAS Aeronautical Journal     Hybrid Journal   (Followers: 30)
Chinese Journal of Aeronautics     Open Access   (Followers: 19)
Ciencia y Poder Aéreo     Open Access   (Followers: 3)
Civil Aviation High Technologies     Open Access   (Followers: 6)
Control Systems     Hybrid Journal   (Followers: 235)
Cosmic Research     Hybrid Journal   (Followers: 5)
Egyptian Journal of Remote Sensing and Space Science     Open Access   (Followers: 25)
Fatigue of Aircraft Structures     Open Access   (Followers: 21)
Frontiers in Aerospace Engineering     Open Access   (Followers: 20)
Frontiers in Astronomy and Space Sciences     Open Access   (Followers: 15)
Gyroscopy and Navigation     Hybrid Journal   (Followers: 177)
IEEE Aerospace and Electronic Systems Magazine     Full-text available via subscription   (Followers: 251)
IEEE Journal on Miniaturization for Air and Space Systems     Hybrid Journal   (Followers: 2)
IEEE Transactions on Aerospace and Electronic Systems     Hybrid Journal   (Followers: 281)
IEEE Transactions on Circuits and Systems I: Regular Papers     Hybrid Journal   (Followers: 43)
International Journal of Aeroacoustics     Hybrid Journal   (Followers: 37)
International Journal of Aerodynamics     Hybrid Journal   (Followers: 46)
International Journal of Aeronautical and Space Sciences     Hybrid Journal   (Followers: 4)
International Journal of Aerospace Engineering     Open Access   (Followers: 86)
International Journal of Aerospace Innovations     Full-text available via subscription   (Followers: 23)
International Journal of Aerospace Psychology     Hybrid Journal   (Followers: 22)
International Journal of Aerospace Sciences     Open Access   (Followers: 36)
International Journal of Applied Geospatial Research     Hybrid Journal   (Followers: 7)
International Journal of Aviation Management     Hybrid Journal   (Followers: 5)
International Journal of Aviation Technology, Engineering and Management     Full-text available via subscription   (Followers: 8)
International Journal of Aviation, Aeronautics, and Aerospace     Open Access   (Followers: 9)
International Journal of Crashworthiness     Hybrid Journal   (Followers: 10)
International Journal of Micro Air Vehicles     Open Access   (Followers: 11)
International Journal of Satellite Communications Policy and Management     Hybrid Journal   (Followers: 15)
International Journal of Space Science and Engineering     Hybrid Journal   (Followers: 13)
International Journal of Space Structures     Full-text available via subscription   (Followers: 19)
International Journal of Space Technology Management and Innovation     Full-text available via subscription   (Followers: 11)
International Journal of Sustainable Aviation     Hybrid Journal   (Followers: 5)
Investigación Pecuaria     Open Access   (Followers: 1)
Journal of Aerodynamics     Open Access   (Followers: 27)
Journal of Aeronautical Materials     Open Access   (Followers: 10)
Journal of Aerospace Engineering     Full-text available via subscription   (Followers: 66)
Journal of Aerospace Engineering & Technology     Full-text available via subscription   (Followers: 22)
Journal of Aerospace Information Systems     Hybrid Journal   (Followers: 27)
Journal of Aerospace Information Systems     Hybrid Journal   (Followers: 57)
Journal of Aerospace Technology and Management     Open Access   (Followers: 10)
Journal of Aircraft     Hybrid Journal   (Followers: 262)
Journal of Aircraft and Spacecraft Technology     Open Access   (Followers: 15)
Journal of Airline and Airport Management     Open Access   (Followers: 11)
Journal of Astrobiology & Outreach     Open Access   (Followers: 5)
Journal of Aviation Technology and Engineering     Open Access   (Followers: 10)
Journal of Aviation/Aerospace Education & Research     Open Access   (Followers: 2)
Journal of Engineering and Technological Sciences     Open Access   (Followers: 2)
Journal of Guidance, Control, and Dynamics     Hybrid Journal   (Followers: 165)
Journal of KONBiN     Open Access   (Followers: 4)
Journal of Navigation     Hybrid Journal   (Followers: 176)
Journal of Propulsion and Power     Hybrid Journal   (Followers: 569)
Journal of Space Safety Engineering     Hybrid Journal   (Followers: 8)
Journal of Space Weather and Space Climate     Open Access   (Followers: 30)
Journal of Spacecraft and Rockets     Hybrid Journal   (Followers: 702)
Journal of Spatial Science     Hybrid Journal   (Followers: 4)
Journal of the American Helicopter Society     Full-text available via subscription   (Followers: 9)
Journal of the Astronautical Sciences     Hybrid Journal   (Followers: 11)
Journal of the Australasian Society of Aerospace Medicine     Open Access   (Followers: 3)
Journal of Wind Engineering and Industrial Aerodynamics     Hybrid Journal   (Followers: 21)
Life Sciences in Space Research     Hybrid Journal   (Followers: 5)
MAD - Magazine of Aviation Development     Open Access   (Followers: 3)
Mekanika : Jurnal Teknik Mesin i     Open Access  
Microgravity Science and Technology     Hybrid Journal   (Followers: 3)
New Space     Hybrid Journal   (Followers: 6)
Nonlinear Dynamics     Hybrid Journal   (Followers: 19)
npj Microgravity     Open Access   (Followers: 3)
Open Aerospace Engineering Journal     Open Access   (Followers: 4)
Perspectives of Earth and Space Scientists i     Open Access   (Followers: 1)
Population Space and Place     Hybrid Journal   (Followers: 10)
Problemy Mechatroniki. Uzbrojenie, lotnictwo, inżynieria bezpieczeństwa / Problems of Mechatronics. Armament, Aviation, Safety Engineering     Open Access   (Followers: 3)
Proceedings of the Human Factors and Ergonomics Society Annual Meeting     Hybrid Journal   (Followers: 16)
Proceedings of the Institution of Mechanical Engineers Part G: Journal of Aerospace Engineering     Hybrid Journal   (Followers: 42)
Progress in Aerospace Sciences     Full-text available via subscription   (Followers: 82)
Propulsion and Power Research     Open Access   (Followers: 89)
REACH - Reviews in Human Space Exploration     Full-text available via subscription   (Followers: 5)
Research & Reviews : Journal of Space Science & Technology     Full-text available via subscription   (Followers: 20)
RocketSTEM     Free   (Followers: 5)
Russian Aeronautics (Iz VUZ)     Hybrid Journal   (Followers: 23)
Science and Education : Scientific Publication of BMSTU     Open Access   (Followers: 1)
Space and Polity     Hybrid Journal   (Followers: 6)
Space Policy     Hybrid Journal   (Followers: 30)
Space Research Today     Full-text available via subscription   (Followers: 43)
Space Safety Magazine     Free   (Followers: 50)
Space Science International     Open Access   (Followers: 117)
Space Science Reviews     Hybrid Journal   (Followers: 92)
SpaceNews     Free   (Followers: 779)
Spatial Information Research     Hybrid Journal   (Followers: 1)
Transactions on Aerospace Research     Open Access   (Followers: 1)
Transport and Aerospace Engineering     Open Access   (Followers: 4)
Transportmetrica A : Transport Science     Hybrid Journal   (Followers: 7)
Unmanned Systems     Hybrid Journal   (Followers: 4)
Xibei Gongye Daxue Xuebao / Journal of Northwestern Polytechnical University     Open Access  
Вісник Національного Авіаційного Університету     Open Access   (Followers: 1)

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Similar Journals
Journal Cover
Gyroscopy and Navigation
Journal Prestige (SJR): 0.292
Citation Impact (citeScore): 1
Number of Followers: 177  
 
  Hybrid Journal Hybrid journal (It can contain Open Access articles)
ISSN (Print) 2075-1087 - ISSN (Online) 2075-1109
Published by Springer-Verlag Homepage  [2469 journals]
  • Study of an Interferometric Fiber-Optic Gyroscope with a Birefringence
           Modulator

    • Free pre-print version: Loading...

      Abstract: The paper describes an interferometric fiber-optic gyroscope (IFOG) of a new configuration, i.e., with a birefringence modulator (IFOG-BRM) is proposed. According to the proposed scheme, a prototype model of the device has been assembled and tested to estimate its drift on a stationary base. Dependence of the IFOG-BRM drift on the temperature has been determined. According to the test results, the error of angular rate estimation is 0.05 deg/h; however, high sensitivity of the device to the absolute temperature variations has been revealed.
      PubDate: 2021-12-01
       
  • Estimation of Error Model Parameters for a Rotating FOG-Based Measurement
           Unit of a Strapdown INS on a Vehicle

    • Free pre-print version: Loading...

      Abstract: The paper studies the possibility of updating the parameters of error model of a rotating inertial measurement unit (IMU) with fiber-optic gyroscopes (FOG) in a strapdown inertial navigation system (SINS) under operating conditions. The IMU is placed in a two-axis gimbal for modulation rotation. The main focus is made on the estimation of scale factor errors of the FOG and accelerometers, non-orthogonality of their sensitive axes, and relative time delays (group delays) of inertial sensors during the IMU normal rotation according to the navigation solution of the INS in the observation mode of its operation. Also, the paper presents the description and results of estimation of so-called rhumb drifts of the IMU, which may occur due to the perturbing forces associated with the geographical axes or the axes of the system central device body. The research is based on the results of FOG-based INS simulation.
      PubDate: 2021-12-01
       
  • Interplanetary Small-Satellite Missions: Ballistic Problems and Their
           Solutions1

    • Free pre-print version: Loading...

      Abstract: — The past decade has been marked by an explosive growth in the number of missions with the use of small spacecraft weighing only about tens of kilograms, including CubeSats that are currently widely employed in various applications. For a scientific paper, it is no longer feasible to enumerate and properly analyze the accomplished missions as well as those under development and being planned: information changes so quickly that perhaps only websites with inline renovations can keep track of all the changes in this market. Near-Earth missions of CubeSats increasingly become the prerogative of engineers and production managers. Nowadays, even factories are built to mass-produce small spacecraft. However, interplanetary small-spacecraft missions stand apart because the technologies used to develop large spacecraft for interplanetary missions are not fully applicable to small spacecraft. The same is true of the ballistic aspects of such missions. This is primarily due to the low energy capability of small spacecraft for maneuvering and transmitting signals over long distances. The other equally important aspects are their self-sufficiency, navigation support, and radiation resistance in outer space. From the standpoint of the scientific novelty of the problems that spacecraft have to face and the fundamentals of ballistic implementation, it is interplanetary missions that attract attention of researchers. This paper discusses the opportunities for interplanetary transportation of small spacecraft and formulates the problems that need to be solved in the near future.
      PubDate: 2021-12-01
       
  • Preventing Resonant Motion Modes for Low-Altitude CubeSat Nanosatellites

    • Free pre-print version: Loading...

      Abstract: Resonant modes of motion, manifested as a significant increase in the oscillation amplitude of the spatial angle of attack, can result in the failure of the CubeSat mission. This paper is concerned with the study of the resonant motion modes of aerodynamically stabilized CubeSat nanosatellites in low circular orbits with small inertia and mass asymmetry. In contrast to axisymmetric bodies of rotation, resonances in CubeSat nanosatellites can be caused not only by small asymmetry, but they also arise due to the form factor of the rectangular parallelepiped. Formulas have been obtained to determine the critical values of the nanosatellite longitudinal angular velocity at which the conditions for the emergence of resonant motion modes are fulfilled. An approach is proposed to prevent possible resonances for CubeSat nanosatellites.
      PubDate: 2021-12-01
       
  • Thermal Zero Drifts in Magneto-Optical Zeeman Laser Gyroscopes

    • Free pre-print version: Loading...

      Abstract: The paper is devoted to the current problem of increasing the accuracy of magneto-optical laser gyros while maintaining their stable operation in real operating conditions. The problem is considered and studied by the example of the magneto-optical Zeeman laser gyroscope, which is one of the effective types of laser gyroscopes. The development and improvement of the technology for creating this type of gyroscopes makes it possible to significantly reduce the sources of the gyroscope zero drift and yet, retain the other properties and performance parameters. The study and validation of the possibility of a significant reduction in the gyroscope key control currents, such as the pumping currents of the active medium and the control currents of frequency bias, will increase the measuring accuracy of the gyroscope and, accordingly, the accuracy of navigation systems based on them.
      PubDate: 2021-12-01
       
  • x-RIO: Radar Inertial Odometry with Multiple Radar Sensors and Yaw Aiding

    • Free pre-print version: Loading...

      Abstract: Abstract A robust and accurate real-time navigation system is crucial for autonomous robotics. In particular, GNSS denied and poor visual conditions are still very challenging as vision based approaches tend to fail in darkness, direct sunlight, fog, or smoke. Therefore, we are taking advantage of inertial data and FMCW radar sensors as both are not affected by such conditions. In this work, we propose a framework, which uses several 4D mmWave radar sensors simultaneously. The extrinsic calibration of each radar sensor is estimated online. Based on a single radar scan, the 3D ego velocity and optionally yaw measurements based on Manhattan world assumptions are fused. An extensive evaluation with real world datasets is presented. We achieve even better accuracies than state of the art stereo Visual Inertial Odometry (VIO) while being able to cope with degraded visual conditions and requiring only very little computational resources.
      PubDate: 2021-12-01
       
  • Improved Inertial Navigation With Cold Atom Interferometry

    • Free pre-print version: Loading...

      Abstract: This article discusses chances and challenges of using cold atom interferometers in inertial navigation. The error characteristics of the novel sensor are presented, as well as one option for an online estimation of the different readout errors. An extended Kalman filter framework is derived and analysed which uses the readout of the atom interferometer as observation in order to correct several systematic errors of a conventional IMU, allowing for an improved strapdown calculation in an arbitrary target system. The performance gain is discussed analytically based on the steady state variances of the filter, as well as on the example of a simulated scenario for Earth orbit satellites. The correction of the conventional IMU errors is further demonstrated in an experiment under laboratory conditions with a higher class sensor emulating an atom interferometer. While the application of the novel technology as a gyroscope is still limited, as pointed out in the paper, the presented framework yields options for a full six degree of freedom operation of the atom interferometer.
      PubDate: 2021-12-01
       
  • Polynomial Filtering Algorithm Applied to Navigation Data Processing under
           Quadratic Nonlinearities in System and Measurement Equations. Part 2.
           Solution Examples

    • Free pre-print version: Loading...

      Abstract: In the first part of the paper, a polynomial filter has been proposed for filtering under quadratic nonlinearities both in the system and measurement equations. The second part details its features and advantages over the extended Kalman filter and illustrates them using a methodological example and examples of navigation data processing.
      PubDate: 2021-12-01
       
  • From the R-7 Missile and the First Manned Mission into Space up to
           Permanently Manned Orbital Station

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      Abstract: Abstract—The paper presents a brief history of preparation for, and execution of, the first manned mission on Vostok spacecraft. The key tasks and challenges met to make this historical event possible are discussed. Further achievements of Russian manned space missions are presented, including the world’s first orbital station Salyut built and launched in orbit 50 years ago. The role of people in space mission is studied. The in-orbit challenges are discussed, as well as their solutions that were found by the crews and improved the spacecraft safety and performance. Examples of crew operations during the missions of the Salyut orbital stations, Mir orbital facility, and the International Space Station are given to illustrate such challenges. The importance of cosmonauts’ participation in the research and experiments on the orbital stations is demonstrated, and positive examples of such participation are provided.
      PubDate: 2021-07-01
      DOI: 10.1134/S2075108721030032
       
  • Adaptive Unscented Kalman Filter for Tracking GPS signals in the Case of
           an Unknown and Time-Varying Noise Covariance

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      Abstract: A new adaptive unscented Kalman filter (AUKF) is proposed to estimate the radio navigation parameters of a GPS signal tracking system in noisy environments and on a highly dynamic object. The experimental results have shown that the proposed AUKF-based method improves the GPS tracking margin by approximately 8 and 3 dB as compared to the conventional algorithm and the KF-based tracking, respectively. At the same time, the accuracy of Doppler frequency measurements increases as well.
      PubDate: 2021-07-01
      DOI: 10.1134/S2075108721030044
       
  • Electrostatic Gyroscope in Spacecraft Attitude Reference Systems

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      Abstract: 25 years ago, the CSRI Elektropribor proposed to use a gimballess electrostatic gyroscope (ESG) in spacecraft attitude reference systems. The system called BIS-EG passed the first flight tests in 2004. By 2013, 20 such systems had been manufactured for spacecraft of three types. The flight tests and regular operation of BIS-EG revealed a number of limitations inherent in them; at the same time, calibration methods were developed and tested and the ways of improving the system accuracy and reliability were identified. As a consequence, BIS-EG was upgraded for the next generation spacecraft, and it is still in operation. The distinctive features of this system are higher reliability, the gyroscope of greater stability, and in-flight calibration of its drift model. The next modification of the BIS-EG, which is under development now, must meet the requirements for higher accuracy characteristics and the need to work in the unpressurized spacecraft compartment. The stages and methods for improving the gimballess ESG and the BIS-EG family systems are described, as well as the results of their operation in accordance with their purposes in spacecraft of different types.
      PubDate: 2021-07-01
      DOI: 10.1134/S2075108721030056
       
  • INS/GNSS Integration with Compensated Data Synchronization Errors and
           Displacement of GNSS Antenna. Experience of Practical Realization

    • Free pre-print version: Loading...

      Abstract: We examine two aspects specific to data fusion of strapdown inertial navigation systems (SINS) aided by global navigation satellite systems (GNSS), with their inherent spatial separation between the GNSS antenna phase center and the inertial measurement unit, as well as with SINS/GNSS synchronization errors. The first aspect refers to modifying the mathematical models used in INS/GNSS integration. The second one relates to our experience in their application in onboard airborne navigation algorithms developed by the Moscow Institute of Electromechanics and Automatics.
      PubDate: 2021-07-01
      DOI: 10.1134/S207510872103007X
       
  • Polynomial Filtering Algorithm Applied to Navigation Data Processing under
           Quadratic Nonlinearities in System and Measurement Equations. Part 1.
           Description and Comparison with Kalman Type Algorithms

    • Free pre-print version: Loading...

      Abstract: The paper considers the filtering problems solved in navigation data processing under quadratic nonlinearities both in system and measurement equations. A Kalman type recursive algorithm is proposed, where the predicted estimate and gain at each step are calculated based on the assumption on the Gaussian posterior probability density function of the estimated vector at the previous step and minimization of estimation error covariance matrices using a linear procedure with respect to the current measurement. The similarities between this algorithm and other Kalman type algorithms such as extended and second-order Kalman filters are discussed. The procedure for evaluating the performance and comparing the algorithms is presented.
      PubDate: 2021-07-01
      DOI: 10.1134/S2075108721030068
       
  • A Fast Search-Free Algorithm for Star Sensor Frame Identification by Star
           Configurations. A Version of Onboard Implementation

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      Abstract: Abstract—The paper presents a method for identifying the frame of a star sensor (SS), based on determination of the star local features allowing its unique recognition. The star identifiers are located in a multidimensional integer feature space, and the relevant feature catalog presents a disperse array, which provides search-free star determination. Examples of onboard implementation of feature catalog are presented, containing the stars up to magnitude of six. The required memory is estimated, and a method is proposed for compressing the feature catalog to be recorded in the onboard computer memory. The frame identification algorithm using the reduced feature catalog is described in detail. The algorithm was tested on real sky frames.
      PubDate: 2021-07-01
      DOI: 10.1134/S2075108721030020
       
  • Automation of Mobile Gravimeter Quartz Elastic System Manufacturing
           Technology

    • Free pre-print version: Loading...

      Abstract: The paper describes an improved technology of quartz elastic system manufacturing for the gravimeters of Chekan series; its purpose is to automate the manufacturing processes of the elastic system elements to improve the work quality and performance. The elastic system manufactured using this technology has been tested on a bench and in field, and the results confirmed its compliance with the requirements set for the sensitive elements of modern mobile gravimeters.
      PubDate: 2021-04-01
      DOI: 10.1134/S2075108721020073
       
  • Numerical Methods of Suboptimal Programs Synthesis for Accelerometer Unit

    • Free pre-print version: Loading...

      Abstract: The paper presents the results of synthesis of calibration programs consisting of 9 and 18 measurement positions. The synthesis was performed by numerical methods for scalar (invariant) technique of accelerometer unit calibration. The resulting programs are compared to the existing calibration programs which have been obtained analytically. The results of mathematical simulation and field experiment confirm the theoretical calculations, as well as the effective application of the obtained calibration programs.
      PubDate: 2021-04-01
      DOI: 10.1134/S2075108721020036
       
  • Design to Operational Parameters Dependency on Quality Factor of Sensor
           Mechanical Resonators

    • Free pre-print version: Loading...

      Abstract: — The critical functional part of any high performance resonance based sensor is a mechanical resonator. The performance is measured by resonator quality factor (Q-factor). Damping mechanisms such as thermoelastic damping (TED), anchor loss, surface loss, material internal friction, fluid damping and electronics damping are covered in this review with more focus on gyroscope resonators. Dissipations can be reduced by different means. Hence, the effects of various design to operational parameters on the Q-factor for different configurations, sizes and materials are reviewed in detail. Micro scale ring resonators can achieve a Q-factor of the order of hundreds of thousands. Macro scale hemispherical resonators are suitable for ultrahigh Q-factors. High temperature sensor operation is not preferred because of TED, while sub-zero operation is limited by material internal friction. Few orders of dissipation increase are seen with thin film metallic coating due to TED and coating material internal friction. High precision fabrication is mandatory to achieve the designed minimum anchor loss as it is highly sensitive to fabrication imperfections. Q-factor sensitivity to operating pressure is different for different resonator configurations. This review study helps to build a comprehensive mechanical resonator design, realization and operation strategy to achieve high sensor performance. A roadmap on future research requirements for developing compact mass producible CVG type sensors with ultrahigh Q-factor is also highlighted.
      PubDate: 2021-04-01
      DOI: 10.1134/S207510872102005X
       
  • A Study on the Effect Produced by Instrumental Error of Automated
           Astronomical System on Landmark Azimuth Accuracy

    • Free pre-print version: Loading...

      Abstract: The paper analyzes how random and systematic components of instrumental error of an automated astronomical system affect the accuracy of the landmark astronomical azimuth. The obtained results can be applied to construct the error mathematical model and to define the mutual orientation of the body axes when designing the system.
      PubDate: 2021-04-01
      DOI: 10.1134/S2075108721020085
       
  • INS/Odometer Integration: Positional Approach

    • Free pre-print version: Loading...

      Abstract: The problem of a strapdown inertial navigation system (SINS) integration with an odometer as part of an integrated navigation system is considered. The odometer raw measurement is considered as an increment of the distance traveled along the odometer “measuring” axis. Models of the integration solution components for the case of three-dimensional navigation are presented, among which are the models of inertial autonomous and kinematic odometer dead reckoning (DR), models of relevant error equations, the model of SINS position aiding based on the odometer DR data and using GNSS position and velocity, wherever possible. The models comprise objective components, which do not depend on the type of the inertial sensors used and their accuracy grade, and variable components, which take into account the properties of the navigation sensors used. The integration does not require zero velocity updates, known as ZUPT correction, which are commonly used in navigation application.
      PubDate: 2021-04-01
      DOI: 10.1134/S2075108721020048
       
  • Gyroscope on de Broglie Waves: Intricate Things in Simple Words

    • Free pre-print version: Loading...

      Abstract: The paper addresses the operating principles of a gyroscopic device of a new type: a gyroscope on de Broglie waves. The sensitive element of such a gyroscope is an atomic interferometer, whose main components are described and the technical challenges of its development are discussed. The target audience of this paper is the readers who do not have a profound knowledge of the quantum physics.
      PubDate: 2021-04-01
      DOI: 10.1134/S2075108721020097
       
 
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