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Inertial Navigation Attitude Measurement System for Uav Navigation Gyroscope

Product Details
Measuring Shaft Quantities: Three
Accuracy Grade: 0.25°
IP Rating: IP67
  • Inertial Navigation Attitude Measurement System for Uav Navigation Gyroscope
  • Inertial Navigation Attitude Measurement System for Uav Navigation Gyroscope
  • Inertial Navigation Attitude Measurement System for Uav Navigation Gyroscope
  • Inertial Navigation Attitude Measurement System for Uav Navigation Gyroscope
  • Inertial Navigation Attitude Measurement System for Uav Navigation Gyroscope
  • Inertial Navigation Attitude Measurement System for Uav Navigation Gyroscope
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  • Overview
  • Product Description
  • Product Parameters
  • Company Profile
  • Company Advantage
  • Our Services
  • Exhibition
  • Packaging & Shipping
  • FAQ
Overview

Basic Info.

Model NO.
INS150A
Certification
CE
Customized
Customized
Heading Accuracy
0.25°
Pitch Accuracy
0.02 °
Rolling Accuracy
0.02 °
Gyro Range
±500°/S
Gyro Zero Bias Stability
≤ 0.11 °/H
Acc Range
±20g
Zero-Bias Repeatability at Room-Temperat
≤ 0.05 °/H
Acc Zero Bias Stability
≤200ug
Power Source
9-36V
Weight
≤0.8kg
Transport Package
Sponge and Box
Specification
78.0mm (L) × 78.0mm (W) × 80.0mm (H)
Trademark
Firepower
Origin
Shenzhen

Product Description

Inertial Navigation Attitude Measurement System for Uav Navigation Gyroscope

Product Description

Inertial Navigation Attitude Measurement System for Uav Navigation Gyroscope
The inertial navigation system is installed on a certain type of carrier, which is mainly used to provide angular rate and linear rate information for the carrier. At the same time, it provides navigation information such as angle, speed and position.
 

 

Product Parameters

1,Accuracy Requirements for Angular Rate Measurement

No. Item Specification
a) Angular rate measurement range ± 500 °/s
b) Zero bias stability (1σ, 10s smooth, RT) ≤ 0.11 °/h
c) Zero bias stability (1σ, 10s smooth, HT/LT) ≤ 0.13 °/h
d) Zero-bias repeatability (1σ, RT) ≤ 0.05 °/h
e) Scale factor non-linearity (RT) ≤ 20ppm
f) Scale factor repeatability (RT) ≤ 20ppm
g) Gyro bandwidth 200Hz (guaranteed by design)
h) Startup time for gyro precision 10s

2, Accuracy Requirements for Linear Velocity Measurement

No. Item Specification
a) Acceleration measurement range ± 20 g (model selection guarantee) (optional 50g product, slightly lower accuracy)
b) Zero bias stability (1σ, 10s smooth, RT) ≤ 200μg
c) Zero-bias repeatability (1σ, RT) ≤ 200μg
d) Startup time 10s

3, Initial Alignment Accuracy Requirement

No. Item Specification
a) Initial alignment modes Rocking base, mooring system, satellite-assisted, odometer (or DVL)-assisted
b) Heading accuracy (rocking base) 0.25 ° · SecL (L = local latitude)
c) Pitch accuracy (rocking base) 0.02 °
d) Roll accuracy (rocking base) 0.02 °
e) Initial alignment time (rocking base) 5min (adaptive adjustment allowed, mooring system recommended 10min)
  Note Alignment accuracy corresponds to specified alignment time

4, Satellite Failure Pure Inertial Navigation Index Requirement

No. Item Specification
a) Heading angle hold accuracy (drift) 0.12 °/h (peak)
b) Pitch angle hold accuracy (drift) 0.1 °/h (peak)
c) Roll angle hold accuracy (drift) 0.1 °/h (peak)
d) Heading angle measurement range 0 ° ~ 360 °
e) Pitch angle measurement range -90 ° ~ + 90 °
f) Roll angle measurement range -180 ° ~ + 180 °
g) Inertial/odometer integrated positioning accuracy 0.6% D (D = driving distance)
h) Pure inertial horizontal positioning accuracy (surface ship mode) 2500 m (peak-to-peak, 1H assessment)
i) Pure inertial horizontal positioning accuracy (ground vehicle mode) 500m (peak-to-peak, 1H assessment)
j) Pure inertial horizontal positioning accuracy (flight vehicle mode) 500m (50% CEP, 10-minute assessment)

5, Requirements for Effective Integrated Navigation of Satellite

No. Item Specification
a) Heading angle accuracy (full maneuver) 0.08 ° (1σ)
b) Pitch angle accuracy (full maneuver) 0.05 ° (1σ)
c) Roll angle accuracy (full maneuver) 0.05 ° (1σ)
d) Horizontal positioning accuracy (satellite single-point, open environment) 1.5m (1σ)
e) Elevation positioning accuracy (satellite single-point, open environment) 2.0m (1σ), supports RTCM3.X (RTK state)
f) Function support Dual-antenna direction finding
g) Function support INS/DVL integrated navigation (DVL access)
h) Function support INS/OD integrated navigation (odometer access)

6, Power Supply Requirements

No. Item Specification
a) Recommended external power supply DC 28V, voltage range 9V ~ 36V
b) Steady-state power consumption ≤ 9W

7,Environmental Adaptability

No. Item Specification
a) Operating temperature range -40 ºC ~ + 60 ºC
b) Storage temperature range -45 ºC ~ + 65 ºC
c) Impact resistance adaptability Not regarded as acceptance item

Inertial Navigation Attitude Measurement System for Uav Navigation Gyroscope

Company Profile

Inertial Navigation Attitude Measurement System for Uav Navigation GyroscopeShenzhen Firepower Control Technology Co., Ltd, was established in 2013 and registered in Shenzhen, The company is high-tech enterprise dedicated to R&D and production of quartz accelerometer, FOG, IMU, INS, Angle testing equipment and other products. The company has invested in and built multiple automated production lines in various locations such as Xi'an, Shenzhen, and Zhuhai. These production lines cover the manufacturing of fiber optic gyroscopes, MEMS inertial navigation systems, quartz accelerometers, electronic countermeasure communication products, and inertial simulation equipment. As an independent innovation-oriented high-tech enterprise, Firepower possesses China's leading production conditions for inertial navigation and electronic countermeasure products. The company always prioritizes scientific research and technological innovation, as well as self-reliance and control. It is committed to developing a series of autonomous navigation products with independent intellectual property rights, which are widely applied in the autonomous navigation perception fields of unmanned aerial vehicles, vehicles, and ships. With its self-developed array algorithm as the core technology, the company has developed a series of inertial navigation products that can provide users' carriers with key information such as current position, three-dimensional attitude, and speed, thereby achieving precise autonomous navigation control.

Inertial Navigation Attitude Measurement System for Uav Navigation Gyroscope

Inertial Navigation Attitude Measurement System for Uav Navigation Gyroscope

Company Advantage

Inertial Navigation Attitude Measurement System for Uav Navigation Gyroscope

Our Services

Inertial Navigation Attitude Measurement System for Uav Navigation Gyroscope

Exhibition

Inertial Navigation Attitude Measurement System for Uav Navigation Gyroscope

Packaging & Shipping

Inertial Navigation Attitude Measurement System for Uav Navigation Gyroscope

FAQ

Q: What is your lead time?
A: Stock: 5-15 days in general. No stock: 15-30 days after samples confirmed. Or please contact us by email for specific lead time based on your order quantities.

Q: How does your factory do regarding quality control?
A: Quality is priority. We always attach great importance to quality control from the very beginning to the end:
1) We produce product according agreed technical requirements strictly;
2) We do full tests according to test methology;
3) We have a professional QA/QC team to ensure the quality.

Q: Do you accept OEM or ODM order?
A: Yes, we are professional manufacturer and we are capable for providing both OEM and ODM service by customer's needs.

Q: What are the terms of delivery?
A: We can accept EXW, FOB, CIF, etc. You can choose one which is the most convenient for you.

Q: What is the payment way?
A: TT, L/C, Pay later, West Union, Online Bank Payment.

Q: What is warranty?
A: Standardly 12 months and negotiable for longer warranty.

Q: What is the packing quality?
A: For sample order, we use carton box with sponge, and batch order, we use wooden box.

Q: What is final price?
A: For standard product, price is as in the price table; For customized product, price by checking with sales, so as to different quantity needs.

Q: How to choose product?
A: We are professional manufacturer, we could provide standard product on shelf, or products by customer's specific requirements:
1) Choose from MadeinChnia platform or website;
2) Customer raise some certain different technical requirements based on standard products;
3) Customer provide specific and comprehensive technical requirements to sales to evaluate;
4) Customer explain application to sales to provide suitable products;

 

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