Introduction
Dynamically Tuned Inertial Navigation System consists of an inertial measurement unit, magnetic heading sensor and control the display, satellite receiving antenna, doppler radar and installation bracket component. The satellite receiving antenna can be 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, acceleration. As the navigation of aircraft, it determines flight control, route management and provides location, velocity, attitude, heading information. Dynamically Tuned Inertial Navigation System has emergency rapid alignment, normal alignment, navigation, correction, parameter calibration, testing, parameter binding and non volatile storage.
Specifications
| Project | ER-DINS-1[1] | ER-DINS-1A[2] | ER-DINS-1N[3] |
| lnertial/Doppler ntegrated NavigationAccuracy- | Position 1%-S,S For The Flying Distance | Position 0.8%-S,S For The Flying Distance | |
| Speed:Not Less Than Doppler Radar Accuracy | Speed:Not less Than Doppler Radar Accuracy | ||
| Heading:0.4°(10) | Heading:0.5°(1σ) | ||
| Atitude:0.2°(1σ) | Atitude:0.2°(1σ) | ||
| Precision of Satellite Navigation | Postion 30m(CEP) | Position 30m(CEP) | Position 30m(CEP) |
| Speed:1m/s(RMS) | Speed:1m/s(RMS) | Speed:0.8m/s(RMS) | |
| Dynamic Adaptability | Angular Velocity≥±100°/S | Angular Velocity≥±100°/S | Angular Velocity≥±100°/S |
| Linear Accelerationz±8g | Linear Accelerationz±8g | Linear Acceleration≥±8g | |
| Angular Acceleration≥200°/S2 | Angular Acceleration≥200/S2 | Angular Acceleration≥300°S2 | |
| Working Temperature | 40℃~+70℃ | 40℃~+65℃ | 40℃~+60℃ |
| Storage Temperature | -55℃~+70℃ | -55℃~+70℃ | -55℃~+70℃ |
| Vibration | 0.0027g2/HZ | 0.02g2/HZ | 0.02g2/HZ |
| Shock | 15g | 15g | 15g |
| Project | ER-DINS-1[1] | ER-DINS-1A[2] | ER-DINS-1N[3] |
| Overall Dimensions | 1/2ATR Standard Case | 1/2ATR Standard Case | 1/2ATR Standard Case |
| 315mm×124mm×194mm | 315mm×124mm×194mm | 315mm×124mm×194mm | |
| Weight | ≤12kg | ≤22.33kg (Containing Doppler Radar) |
≤8.5kg |
| Power Supply | 28VDC Power Consumption≤90W |
28VDC Power Consumption≤65W |
28V DC Power Consumption≤60W |
| Preparation Time (Starting At Normal Temperature) |
Normal Condition 8min Emergency Situation2min |
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:1m/s(RMS) Heading:0.4°(RMS) Attitude:0.2°(RMS) |
| Pure nertial | Position 10km/30min(CEP) | Position 10km/20min(CEP) | Position 1.5nm/10min(CEP) |
| NavigationAccuracy | Speed:6m/s(RMS) Heading:0.4°(RMS) Attitude:0.2°(RMS) |
Speed:5m/s(RMS) Heading:0.4°(RMS) Attitude:0.2°(RMS) |
Speed:6m/s(RMS) Heading:0.5°(RMS) Attitude:0.2°(RMS) |
If you have DHL or Fedex account, we can quote EXW price, otherwise CIF or FOB price.
After we submit the sample price, if more quantity is needed, we will quote the bulk price.
For sensors, parts and modules: in a stock-one week; no stock-2-4 weeks; For systems, generally, 8-12 weeks.
After confirming that the product has quality problems, we will replace it for you free of charge in the shortest possible time.
At here, it’s all about giving the clients thebest quality products.
Beijing Andelu Technology Development Co., Ltd. is a technology-based company dedicated to the development and sales of electronic components.
