Sushchenko, 2021 - Google Patents
Gimballed attitude and heading reference system for marine vehiclesSushchenko, 2021
- Document ID
- 17541087360576886995
- Author
- Sushchenko O
- Publication year
- Publication venue
- 2021 IEEE 3rd Ukraine Conference on Electrical and Computer Engineering (UKRCON)
External Links
Snippet
The paper deals with creating a gimballed attitude and heading system assigned for operation on marine vehicles. Features of the developed system are the high precision and resistance to accelerations. The kinematical scheme of the considered system is …
- 238000004088 simulation 0 abstract description 6
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C21/00—Navigation; Navigational instruments not provided for in preceding groups
- G01C21/10—Navigation; Navigational instruments not provided for in preceding groups by using measurements of speed or acceleration
- G01C21/12—Navigation; Navigational instruments not provided for in preceding groups by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
- G01C21/16—Navigation; Navigational instruments not provided for in preceding groups by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
- G01C21/18—Stabilised platforms, e.g. by gyroscope
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C21/00—Navigation; Navigational instruments not provided for in preceding groups
- G01C21/10—Navigation; Navigational instruments not provided for in preceding groups by using measurements of speed or acceleration
- G01C21/12—Navigation; Navigational instruments not provided for in preceding groups by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
- G01C21/16—Navigation; Navigational instruments not provided for in preceding groups by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
- G01C21/165—Navigation; Navigational instruments not provided for in preceding groups by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation combined with non-inertial navigation instruments
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
- G01C19/02—Rotary gyroscopes
- G01C19/34—Rotary gyroscopes for indicating a direction in the horizontal plane, e.g. directional gyroscopes
- G01C19/38—Rotary gyroscopes for indicating a direction in the horizontal plane, e.g. directional gyroscopes with north-seeking action by other than magnetic means, e.g. gyrocompasses using earth's rotation
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C25/00—Manufacturing, calibrating, cleaning, or repairing instruments and devices referred to in the preceding groups
- G01C25/005—Manufacturing, calibrating, cleaning, or repairing instruments and devices referred to in the preceding groups initial alignment, calibration or starting-up of inertial devices
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
- G01C19/56—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces
- G01C19/5635—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces using vibrating wires or strings
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C21/00—Navigation; Navigational instruments not provided for in preceding groups
- G01C21/20—Instruments for performing navigational calculations
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C17/00—Compasses; Devices for ascertaining true or magnetic north for navigation or surveying purposes
- G01C17/38—Testing, calibrating, or compensating of compasses
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C17/00—Compasses; Devices for ascertaining true or magnetic north for navigation or surveying purposes
- G01C17/02—Magnetic compasses
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN113029199B (en) | A system-level temperature error compensation method for laser gyro inertial navigation system | |
Hong | Fuzzy logic based closed-loop strapdown attitude system for unmanned aerial vehicle (UAV) | |
US4244215A (en) | Autonomous navigation system | |
US7216055B1 (en) | Dynamic attitude measurement method and apparatus | |
US7418364B1 (en) | Dynamic attitude measurement method and apparatus | |
CN103630146B (en) | The laser gyro IMU scaling method that a kind of discrete parsing is combined with Kalman filter | |
Sahawneh et al. | Development and calibration of low cost MEMS IMU for UAV applications | |
CN109752000A (en) | A method for initial alignment of MEMS dual-axis rotational modulation strapdown compass | |
US3269024A (en) | Method and means for aligning an axis on a gimbaled platform | |
Cannon Jr | Alignment of inertial guidance systems by gyrocompassing-linear theory | |
Sushchenko | Gimballed attitude and heading reference system for marine vehicles | |
Sushchenko | Mathematical model of triaxial multimode attitude and heading reference system | |
US3131292A (en) | Coordinate reference system | |
RU2608337C1 (en) | Method of three-axis gyrostabilizer stabilized platform independent initial alignment in horizontal plane and at specified azimuth | |
RU2339002C1 (en) | Method of evaluation of navigation parameters of operated mobile objects and related device for implementation thereof | |
CN111141285A (en) | Aviation gravity measuring device | |
Zhao et al. | A study on alignment of analytic space stable inertial navigation system | |
CN110260862A (en) | A kind of heligyro load navigation device based on Strapdown Inertial Navigation System | |
Akimov et al. | Compensation for errors in determining the angle in the flight-navigation complex of the aircraft in case of failure of the satellite navigation system | |
Sushchenko | Design of Robust Navigation and Stabilization Loops of Precision Attitude and Heading Reference System | |
CN113375694A (en) | Low-cost gyroscope all-zero-offset rapid estimation method under static base condition | |
US3214983A (en) | Attitude reference | |
Sotak | Testing the coarse alignment algorithm using rotation platform | |
Sushchenko | Control of Gimballed Attitude and Heading Reference Systems | |
RU2782334C1 (en) | Method for determining object orientation parameters using semi-analytical inertial navigation system with geographical orientation of four-axis gyroplatform axes |