Dynamically Tuned Gyro INS
Dynamically Tuned Gyro INSDynamically tuned gyro inertial navigation system is by inertial measurement unit, magnetic heading sensor and control the display, satellite receiving antenna, Doppler radar and installation bracket component. The satellite receiving antenna can customized according to the needs for BD2/GPS/GLONASS triple a receiving antenna or BD2 anti-interference antenna.Inertial measurement unit can also be a separate form of inertial measurement unit , for all kinds of missile flight control system and guidance system.Strapdown inertial navigation system determination of aircraft position, heading, altitude, the acceleration, as the navigation of aircraft, flight control, route management provide location, velocity, attitude and heading information. System with emergency rapid alignment, normal alignment, navigation, correction, parameter calibration, testing, parameter binding, non volatile storage.ProjectER-1[1]ER-1A[2]ER-1N[3]Overall Dimensions1/2ATR Standard Case315mm×124mm×194mm1/2ATR Standard Case315mm×124mm×194mm1/2ATR Standard Case315mm×124mm×194mmWeight≤12kg≤22.33kg（Containing Doppler radar）≤8.5kgPower Supply28V DC Power Consumption≤90W28V DC Power Consumption≤65W28V DC Power Consumption≤60WPreparation Time(Starting At Normal Temperature)Normal Condition 8minEmergency Situation 2minNormal Condition 8minEmergency Situation 3minNormal Condition 6minEmergency Situation 3minPrecision Of Integrated Navigation Position: 30m(CEP)Speed: 1m/s(RMS)Heading: 0.4°(RMS)Attitude: 0.2°(RMS)Position: 30m(CEP)Speed: 1m/s(RMS)Heading: 0.4°(RMS)Attitude: 0.2°(RMS)Position: 30m(CEP)Speed: 0.5m/s(RMS)Heading: 0.4°(RMS)Attitude: 0.2°(RMS)Pure Inertia Navigation Accuracy Position: 10km/30min(CEP)Speed: 6m/s(RMS)Heading: 0.4°(RMS)Attitude: 0.2°(RMS)Position: 10km/20min(CEP)Speed: 5m/s(RMS)Heading: 0.4°(RMS)Attitude: 0.2°(RMS)Position: 1.5nm/10min(CEP)Speed: 6m/s(RMS)Heading: 0.5°(RMS)Attitude: 0.2°(RMS)Inertial / Doppler Integrated Navigation Accuracy -Position: 1%·S,S For The Flying DistanceSpeed: Not Less Than Doppler Radar AccuracyHeading: 0.4°(1σ)Attitude: 0.2°(1σ)Position: 0.8%·S,S For The Flying DistanceSpeed: Not less Than Doppler Radar AccuracyHeading: 0.5°(1σ)Attitude: 0.2°(1σ)Precision Of Satellite Navigation Position: 30m(CEP)Speed: 1m/s(RMS)Position: 30m(CEP)Speed: 1m/s(RMS)Position: 30m(CEP)Speed: 0.8m/s(RMS)Dynamic Adaptability Angular Velocity ≥±100°/SLinear Acceleration ≥±8gAngular Acceleration≥200°/S2Angular Velocity ≥±100°/SLinear Acceleration ≥±8gAngular Acceleration≥200°/S2Angular Velocity ≥±100°/SLinear Acceleration≥±8gAngular Acceleration ≥300°/S2Working Temperature -40ºC~+70℃-40ºC~+65℃-40ºC~+60℃Storage Temperature -55ºC~+70℃-55ºC~+70℃-55ºC~+70℃Vibration0.0027g2/HZ0.02g2/HZ0.02g2/HZShock15g15g15gNote[1] : contains the control display. Note [2] : contains Doppler radar. Note [3]: with moving base alignment and DVS current correction function.ERICCO is expert in high quality dynamically tuned gyro ins manufacturing and selling, who is one of the best manufacturers and suppliers of dynamically tuned gyro ins with high precision. We have a professional factory at your service.
Other supplier products
|
|
|
High temperature memoryl Name: high temperature flash memoryl With high temperature, small volume, large density, fast reading rate and rare erro... |
|
|
|
ER-102 High precision AntennaER-102 with precise positioning and navigation compass has excellent directional performance experience. The use of Ve... |
|
|
|
Signal Analog DeviceNS series satellite Signal analog device is based on CPCI structure, can achieve GPS, GLONASS, BD1 navigation system satellite... |
|
|
|
NS-FGI1100 Fiber optic inertial navigation systemFGI1100 Inertial navigation system using triaxial fiber optic gyro sensitive vector angular motion... |
|
|
|
ER132A Three Axis Laser GyroscopeThe model is integrated two laser gyro component and a single axis laser gyro small groups of three axis laser gyr... |
供应产品
Same products
