CN106248104A - A kind of north finder comprehensive slewing and torque compensation method - Google Patents
A kind of north finder comprehensive slewing and torque compensation method Download PDFInfo
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- CN106248104A CN106248104A CN201610532456.1A CN201610532456A CN106248104A CN 106248104 A CN106248104 A CN 106248104A CN 201610532456 A CN201610532456 A CN 201610532456A CN 106248104 A CN106248104 A CN 106248104A
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- constant value
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- 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 or devices referred to in the other groups of this subclass
- G01C25/005—Manufacturing, calibrating, cleaning, or repairing instruments or devices referred to in the other groups of this subclass initial alignment, calibration or starting-up of inertial devices
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- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
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- Gyroscopes (AREA)
Abstract
The invention belongs to inertia and seek north orientation survey technical field, be specifically related to a kind of by north finder gyrocompassing backoff algorithm, improve the comprehensive slewing of north finder and the torque compensation method seeking north orientation survey precision.The present invention includes: the quick low precision of magnetic compass orients;± 1 ° of two-position orientation;Three position compensation conductive hairspring disturbance torques.The present invention solves the demand of the multiple application of above-mentioned north finder device, on the premise of not changing main body instrument and hardware, propose and devise two-position slewing and compensate the algorithm of guide's silk disturbance torque, to realize improving orientation system precision, meeting quick corresponding demand.
Description
Technical field
The invention belongs to inertia and seek north orientation survey technical field, be specifically related to one and mended by north finder gyrocompassing
Repay algorithm, improve the comprehensive slewing of north finder and the torque compensation method seeking north orientation survey precision.
Background technology
Now with the development of Defense Weapon System, north finder is sought north time, orientation accuracy and requires more and more higher.With
Time, along with the complication of weaponry environment, general north finder orientation method realizes seeking north by rotating 180 °, but
Some special external environment can limit its angle rotated, and causes seeking north error and increases even failed, on the other hand, bigger
The anglec of rotation can increase seeks the north time, affects the rapidity of system.
Summary of the invention
It is an object of the invention to provide a kind of magnetic compass quick low precision orientation, two-position of introducing high-precision fixed to calculation
Method, north finder comprehensive slewing and the torque compensation method of three position compensation conductive hairspring disturbance torque algorithms
The object of the present invention is achieved like this:
(1) magnetic compass quick low precision orientation
Demarcated the angle of gyro motor axle and north orientation by magnetic compass, gyro service precision reaches 0.5 °, by gyro installation
The angle of gyro machine axle and north orientation is given in systems in 10s;
(2) ± 1 ° of two-position orientation
On the basis of magnetic compass coarse positioning, north finder is carried out little scope ± 1 ° and rotates, it is thus achieved that measure position, position for two
Put 1 and position 2, by the dynamic balance feedback current measured in torquer stator, rotor for twice, calculate the constant value moment recorded
Value, and then calculate the angle of gyro machine axle and north orientation;.
(3) three position compensation conductive hairspring disturbance torques
Orientation system initial position is north orientation, when its rotation alpha angle, and in-position 2,
Orient by initial position rotate-α angle, in-position 3,
In formula: MKFor the control moment measured;HGFor rotation momentum, its unit is Kg m2/ s thousand;ωieFor the earth certainly
Tarnsition velocity, its value is 72.9211 × 10-6rad/s;For local geographic latitude;α is angle between gyroaxis and north orientation;
M2 Constant value moment, M3 Constant value momentConstant value moment for position of rotation 2 with position 3;
The constant value moment of north finder is:
Wherein: M1 Constant value momentConstant value moment for position of rotation 1;
Due to the existence of disturbance torque,
M2 Constant value moment=MConstant value moment+ Δ M, M3 Constant value moment=MConstant value moment-Δ M,
Disturbance torque is:
Δ M=M3 Constant value moment-M2 Constant value moment,
Being compensated directional angle is:
Δ α is i.e. the compensation to guide's silk disturbance torque.
The beneficial effects of the present invention is:
The present invention solves the demand of the multiple application of above-mentioned north finder device, in the premise not changing main body instrument and hardware
Under, propose and devise two-position slewing and compensate the algorithm of guide's silk disturbance torque, to realize improving orientation system essence
Degree, meets the demand of quickly response.
Accompanying drawing explanation
Fig. 1 is that the north finder of patent of the present invention rotates schematic diagram.
Fig. 2 is the particular flow sheet of the present invention.
Specific implementation method
Below in conjunction with the accompanying drawings the present invention is described further:
After north finder starts, carry out fast rough with magnetic compass, make north finder navigate to position 1;Then one is rotated
Low-angle α, makes north finder in-position 2, to carry out data acquisition in position 1 and position 2 respectively, carries out seeking north calculating, is sought
North instrument seek north moment;Rotate north finder to-α, i.e. position 3, by 3 position torque analysis, available caused by silk of conducting a sightseeing tour
Disturbance torque, then can calculate the offset angle compensated required for this moment, to improve system accuracy.
1, magnetic compass quick low precision orientation
Under comprehensive state, the orientation moment experienced due to gyro sensitive element is different, causes measuring range relatively big,
This just brings the polynomial system deviations such as force feedback loop, for reducing system approach error as far as possible, need to predict gyro as far as possible
Motor drive shaft and the angle of north orientation, along with the raising of geomagnetic sensor precision, the magnetic compass that cost performance is higher obtains in multiple fields
Having arrived application, through the demarcation to magnetic compass, its service precision reaches 0.5 °, and being installed by this sensor in systems can be
The angle of gyro machine axle and north orientation is given, first with it as the thickest orientation sensor in the present invention, for rear in 10s
Continuous high-acruracy survey creates fasting conditions.
2, little scope (± 1 °) two-position orientation algorithm
On the basis of magnetic compass coarse positioning, north finder is carried out little scope rotation, it is thus achieved that measure position, position 1 for two
With position 2, by the dynamic balance feedback current in twice measurement torquer stator, rotor, calculate the constant value moment values recorded,
And then calculate the angle of gyro machine axle and north orientation, reach to orient purpose.This process employs two-position oriented solution to calculate calmly
To moment, thus resolving the angle of gyro machine axle and north orientation, usually, orientation time is not more than 5 minutes, and this orientation time wraps
Time, force feedback loop equilibration time, sampling time, rotational time etc. are floated containing motor starting time, magnetic.
3, three position compensation conductive hairspring disturbance torque
North finder applies rotor case sensing assembly, for completing transmission and the power supply of signal, have employed disturbance torque relatively
Few guide's silk device, has the shadows such as the dependency with corner, gyroscopic procession moment, system decorating position due to its disturbance torque
Ringing, cause the center balance point position of the equilibrium point not conductive hairspring of force feedback loop, this just causes conductive hairspring interference
The existence of moment, this error and the material of conductive hairspring, install, the process control procedure such as welding relevant, but its necessary being, but
It has symmetry, uses corner mode can offset its impact.
Assume that orientation system initial position is north orientation, when its rotation alpha angle, in-position 2, obtain equation below:
Orient and rotated-α angle, in-position 3 by initial position, obtain equation below:
In formula: MKFor the control moment measured;HGFor rotation momentum, its unit is Kg m2/ s thousand;ωieFor the earth certainly
Tarnsition velocity, its value is 72.9211 × 10-6rad/s;For local geographic latitude;α is angle between gyroaxis and north orientation;
M2 Constant value moment, M3 Constant value momentConstant value moment for position of rotation 2 with position 3.
The constant value moment of north finder is:
Wherein: M1 Constant value momentConstant value moment for position of rotation 1.
Due to the existence of disturbance torque, M2 Constant value moment=MConstant value moment+ Δ M, M3 Constant value moment=MConstant value moment-Δ M, it can thus be appreciated that perturbed force
Square:
Δ M=M3 Constant value moment-M2 Constant value moment
So, can obtain compensation directional angle is:
Δ α is i.e. the compensation to guide's silk disturbance torque.
Claims (1)
1. a north finder comprehensive slewing and torque compensation method, it is characterised in that comprise the steps:
(1) magnetic compass quick low precision orientation
Demarcated the angle of gyro motor axle and north orientation by magnetic compass, gyro service precision reaches 0.5 °, by gyro installation is being
System is given in 10s the angle of gyro machine axle and north orientation, quickly provides the north orientation of coarse positioning;
(2) ± 1 ° of two-position orientation
On the basis of magnetic compass coarse positioning, north finder is carried out little scope ± 1 ° and rotates, it is thus achieved that measure position, position 1 for two
With position 2, by the dynamic balance feedback current in twice measurement torquer stator, rotor, calculate the constant value moment values recorded,
And then calculate the angle of gyro machine axle and north orientation;
(3) three position compensation conductive hairspring disturbance torques
Orientation system initial position is north orientation, when its rotation alpha angle, and in-position 2,
Orient by initial position rotate-α angle, in-position 3,
In formula: MKFor the control moment measured;HGFor rotation momentum, its unit is Kg m2/ s thousand;ωieFor earth rotation angle
Speed, its value is 72.9211 × 10-6rad/s;For local geographic latitude;α is angle between gyroaxis and north orientation;M2 Constant value moment,
M3 Constant value momentConstant value moment for position of rotation 2 with position 3;
The constant value moment of north finder is:
Wherein: M1 Constant value momentConstant value moment for position of rotation 1;
Due to the existence of disturbance torque,
M2 Constant value moment=MConstant value moment+ Δ M, M3 Constant value moment=MConstant value moment-Δ M,
Disturbance torque is:
Δ M=M3 Constant value moment-M2 Constant value moment,
Being compensated directional angle is:
Δ α is i.e. the compensation to guide's silk disturbance torque.
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CN201610532456.1A CN106248104A (en) | 2016-07-07 | 2016-07-07 | A kind of north finder comprehensive slewing and torque compensation method |
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CN201610532456.1A CN106248104A (en) | 2016-07-07 | 2016-07-07 | A kind of north finder comprehensive slewing and torque compensation method |
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108827273A (en) * | 2018-03-30 | 2018-11-16 | 湖北三江航天万峰科技发展有限公司 | A kind of micro-torque signal transmitting apparatus |
CN110108265A (en) * | 2019-04-25 | 2019-08-09 | 长安大学 | A kind of gyro to measure instrument in autonomous acquisition geographic latitude and automatic seeking north |
CN111089574A (en) * | 2019-12-26 | 2020-05-01 | 陕西宝成航空仪表有限责任公司 | Small-sized rotor gyroscope with power transmission device and small-angle working range |
CN115615465A (en) * | 2022-12-19 | 2023-01-17 | 西安航天精密机电研究所 | Conductive hairspring interference torque adjustable liquid-floated gyroscope and test adjusting method thereof |
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DE3541848A1 (en) * | 1985-11-27 | 1987-06-04 | Teldix Gmbh | North-seeking gyroscope device |
CN103376098A (en) * | 2012-04-27 | 2013-10-30 | 中国人民解放军第二炮兵工程学院 | Automatic latitude measuring and calculating and automatic precision compensating method of pendulum gyro north seeker |
CN103512570A (en) * | 2013-10-12 | 2014-01-15 | 北京信息科技大学 | Preset 45-degree north-seeking method with calculation failure determination |
CN103822624A (en) * | 2014-03-12 | 2014-05-28 | 西安北方捷瑞光电科技有限公司 | Uniaxial laser gyro north seeker and north-seeking method thereof |
CN104266647A (en) * | 2014-09-02 | 2015-01-07 | 北京航天发射技术研究所 | Rapid anti-disturbance north finding instrument based on transposition north finding technology and north finding method |
CN105136163A (en) * | 2015-07-31 | 2015-12-09 | 长安大学 | Magnetically suspended gyroscope north-seeking data gross error rejecting method based on double position characteristics |
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2016
- 2016-07-07 CN CN201610532456.1A patent/CN106248104A/en active Pending
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
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DE3541848A1 (en) * | 1985-11-27 | 1987-06-04 | Teldix Gmbh | North-seeking gyroscope device |
CN103376098A (en) * | 2012-04-27 | 2013-10-30 | 中国人民解放军第二炮兵工程学院 | Automatic latitude measuring and calculating and automatic precision compensating method of pendulum gyro north seeker |
CN103512570A (en) * | 2013-10-12 | 2014-01-15 | 北京信息科技大学 | Preset 45-degree north-seeking method with calculation failure determination |
CN103822624A (en) * | 2014-03-12 | 2014-05-28 | 西安北方捷瑞光电科技有限公司 | Uniaxial laser gyro north seeker and north-seeking method thereof |
CN104266647A (en) * | 2014-09-02 | 2015-01-07 | 北京航天发射技术研究所 | Rapid anti-disturbance north finding instrument based on transposition north finding technology and north finding method |
CN105136163A (en) * | 2015-07-31 | 2015-12-09 | 长安大学 | Magnetically suspended gyroscope north-seeking data gross error rejecting method based on double position characteristics |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108827273A (en) * | 2018-03-30 | 2018-11-16 | 湖北三江航天万峰科技发展有限公司 | A kind of micro-torque signal transmitting apparatus |
CN108827273B (en) * | 2018-03-30 | 2020-06-19 | 湖北三江航天万峰科技发展有限公司 | Micro-torque signal transmission device |
CN110108265A (en) * | 2019-04-25 | 2019-08-09 | 长安大学 | A kind of gyro to measure instrument in autonomous acquisition geographic latitude and automatic seeking north |
CN110108265B (en) * | 2019-04-25 | 2022-11-18 | 长安大学 | Gyro measuring instrument capable of autonomously acquiring geographic latitude and automatically searching north |
CN111089574A (en) * | 2019-12-26 | 2020-05-01 | 陕西宝成航空仪表有限责任公司 | Small-sized rotor gyroscope with power transmission device and small-angle working range |
CN111089574B (en) * | 2019-12-26 | 2023-11-10 | 江苏大发建设工程有限公司 | Small rotor gyroscope with power transmission device and small-angle working range |
CN115615465A (en) * | 2022-12-19 | 2023-01-17 | 西安航天精密机电研究所 | Conductive hairspring interference torque adjustable liquid-floated gyroscope and test adjusting method thereof |
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