Attitude Heading Reference System Microelectromechanical Systems Small Volume and Weight|selectable Interface|high Accuracy|static|dynamnic|proven Technology|used In Demanding Conditions for Unmanned Aerial Vehicle (MEMS AHRS)

Attitude Heading Reference System Microelectromechanical Systems Small Volume and Weight|selectable Interface|high Accuracy|static|dynamnic|proven Technology|used In Demanding Conditions for Unmanned Aerial Vehicle (MEMS AHRS)

1. Auto-output of navigation info.
2. Accurate measurement in large maneuver flight and hovering.
3. Small volume and weight.
4. RS422、CAN, to be selectable.
5. Wide voltage input range.
6. Can complete redevelopment.
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Product Details

Attitude Heading Reference System Microelectromechanical Systems Small Volume And Weight|selectable Interface|high Accuracy|static|dynamnic|proven Technology|used In Demanding Conditions For Unmanned Aerial Vehicle (MEMS AHRS)


1. Brief introduction


TY421 type MEMS AHRS is R & D by the Xi'an Jierui. This product uses MEMS gyro and MEMS accelerometer, as well as a mature attitude calculation algorithm, can autonomously complete the attitude calculation function in harsh environmental conditions, can also provide heading by being combined with dual antenna GPS or magnetometer. And the combination of dual antenna GPS can continuously and real-time provide the instant position (longitude and latitude), velocity, acceleration, heading and attitude of the aircraft.


2. Features


(1) Auto-output  of navigation information

(2) Meet the requirement of accurate measurement of attitude angle of aircraft, when in large maneuver flight and hovering.

(3) Small volume and weight.

(4) Communication interface RS422、CAN, to be selectable.

(5) Wide voltage input range.

(6) Can complete redevelopment according to customers’ requirement.


3. Performances


Sr. No.

Item

Grade

Remark

 System

1

Preparation time

≤2min

2

Attitude accuracy

≤1°   1σ (static)

≤2°   1σ (dynamic)

3

Heading accuracy

≤0.2°/ Baseline(GPS combined)

≤0.5°Magnetometer combined

4

Height accuracy

10 m (GPS combined)

5

Horizontal position accuracy

10m (CEP)(GPS combined)

6

Velocity accuracy

0.02m/s  (GNSS combined)

Environment suitability

7

Shock

30g

8

Working temperature

-40℃~65℃

9

Vibration

Meet the vehicle vibration requirement of GJB150.16A-2009

Physics characteristics

10

Size

150*110*50mm

11

Weight

<700g

12

Power supply

18VDC~36VDC

13

Working power dissipation

10W

Interface characteristics

14

Interface

RS232、RS422、CAN

Selectable

15

MTBF

≥1500h


16

Data refresh rate

100Hz


17

Band rate

115200bps


18

Memory

32G

customized

                      

4. Applications


(1) Unmanned aerial vehicle

(2) Unmanned surface vessel

(3) Counter-terrorism, search for and rescue.

(4) Robots, unmanned vehicles

201706151129438882912.jpg


5. Packages


inertial navigation system package.jpg  inertial navigation packing.jpg



E-mail: info@gyro-nav.com


If you are interested in the attitude heading reference system microelectromechanical systems small volume and weight|selectable interface|high accuracy|static|dynamnic|proven technology|used in demanding conditions for unmanned aerial vehicle (mems ahrs), consult the price with our manufacturers in China now. With advanced technology, our products take high accuracy, high precision, high sensitivity, high reliability, high performance, high stability and low cost as main advantages.

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