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ER-Dynamically Tuned Inertial Navigation System

Features:
1. Strapdown inertial navigation system determination of aircraft position, heading, altitude;
2. System with emergency rapid alignment, normal alignment, navigation, correction, parameter calibration, testing, parameter binding, non volatile storage.

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ER-Dynamically Tuned Inertial Navigation System


Flexible Strapdown Inertial Integrated Navigation System


Dynamically Tuned Inertial Navigation System.jpg


Product features

Strapdown inertial navigation system consists of 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 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 determines aircraft position, heading, altitude, the acceleration. As the navigation of aircraft, it determines flight control, route management and provides location, velocity, attitude, heading information. This system has emergency rapid alignment, normal alignment, navigation, correction, parameter calibration, testing, parameter binding and non volatile storage.



Project

ER-1[1]

ER-1A[2]

ER-1N[3]

Overall Dimensions

1/2ATR Standard Case

315mm×124mm×194mm

1/2ATR Standard Case

315mm×124mm×194mm

1/2ATR Standard Case

315mm×124mm×194mm

Weight

≤12kg

≤22.33kgContaining Doppler radar

≤8.5kg

Power Supply

28V DC Power Consumption≤90W

28V DC Power Consumption≤65W

28V DC Power Consumption≤60W

Preparation TimeStarting At Normal Temperature

Normal Condition 8min

Emergency Situation 2min

Normal Condition 8min

Emergency Situation 3min

Normal Condition 6min

Emergency Situation 3min

Precision 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 Distance

Speed:Not Less Than Doppler Radar Accuracy

Heading:0.4°(1σ)

Attitude:0.2°(1σ)

Position:0.8%·S,S For The Flying Distance

Speed:Not less Than Doppler Radar Accuracy

Heading: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°/S

Linear Acceleration ≥±8g

Angular Acceleration≥200°/S2

Angular Velocity ≥±100°/S

Linear Acceleration ≥±8g

Angular Acceleration≥200°/S2

Angular Velocity ≥±100°/S

Linear Acceleration≥±8g

Angular Acceleration ≥300°/S2

Working Temperature

 

-40ºC~+70℃

-40ºC~+65℃

-40ºC~+60℃

Storage Temperature

 

-55ºC~+70℃

-55ºC~+70℃

-55ºC~+70℃

Vibration

0.0027g2/HZ

0.02g2/HZ

0.02g2/HZ

Shock

15g

15g

15g

Note: [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 flexible strapdown inertial integrated navigation system manufacturing and selling, who is one of the best manufacturers and suppliers of flexible strapdown inertial integrated navigation system with high precision. We have a professional factory at your service.


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