AHRS-002
    Publish time 2016-09-08 13:38    
AHRS-002 integrates INS / GPS, AHRS heading and attitude reference system, flight control system, to meet the MIL-SPEC environmental requirements.
AHRS-002
AHRS-002

Today's unmanned aerial vehicles and military applications require highly sophisticated, compact and cost-effective inertial navigation systems. Yach engineers designed the AHRS-002 inertial navigation system to meet these requirements, providing a comprehensive solution to the flight control system  and MIL-SPEC environmental requirements, including temperature, shock, vibration, electromagnetic interference, power and humidity, etc., to meet the harsh flight environment, and provide our customers with a variety of solutions and make the products in the shortest possible time with the lowest Lifecycle costs go to market.

Advantages:
1. Using the highest IMU inertial measurement system (1, 2 or 3 ° / hour)
2. Using the WAAS Differential Prep GPS receiver
3. Built-in air data system pressure sensor, including static, airspeed and flow angle measurement
4. Supporting all INS attitude solutions
5. Providing accurate roll and pitch data, continuous turning in dynamic and mobile environment.
6. The Kalman filter INS to provide high-precision navigation and control of state vectors

Parameters

SPECIFICATIONS

INS/GPS performance

Update rate

100 Hz only

Start-up time

10 sec (initial attitude);

1 min (full alignment)

Heading range

+/- 180°

Attitude range pitch

+/- 90°

Attitude range roll

+/- 180°

Altitude range

-1,000 ft to 50,000 ft

Baroinertial altitude accuracy

45 ft at S.L., 300 ft at >

40,000 ft altitude

GPS range

Worldwide

Lat/long position accuracy  

GPS receiver accuracy

Max airspeed

165 knots standard,

up to 650 knots available

IMU performance (HG1700)

Rate gyro bias

1 or 3 deg/hr

Maximum g range

Maximum angular rates

Environmental Specifications

Operating Temperature

-40 to 70 

Serial input/output

(2) RS-232>

(2) RS-422>

(1) RS-422  DGPS>

(1) RS-422  Service Port

Temperature shock

MIL-STD-810

Operating temperature at altitude

MIL-STD-810

 

Operating vibration/shock

MIL-STD-810

Sand and dust, salt, fog, fungus

MIL-STD-810 (sealed enclosure

Acceleration/mechanical shock

MIL-STD-810

Humidity

95%, non-condensing

sealed enclosure