IMU-001 integrates INS / GPS, atmospheric data suite and multi-variable control algorithm.
Description:
The IMU-001 inertial navigation system is designed by Yach engineers with a fully integrated and miniaturized flight control system that incorporates INS / GPS and a complete suite of powerful atmospheric data and multivariable control algorithms. The IMU-001 utilizes the LTi'zation design technology specifically designed for high-performance, unmanned systems and provides sophisticated flight control algorithms for a variety of applications.
Advantages:
1. GPS / INS navigation integrated system solution to solve the most advanced multi-input / multiple output of the flight control law
2. Product airspeed control mode including altitude, climb rate, angle of attack, side slip, three-dimensional car navigation and automatic takeoff / landing
3. Utilizing highly reliable solid state sensors including accelerometer, rate Gyroscope, magnetometer, atmospheric data kit and differential prepare along AOA and SLV sensors, enabling WAAS-GPS to receive a complete INS / GPS navigation
Parameters:
SPECIFICATIONS
INS/GPS performance
Update rate
100 Hz
Start-up time
10 sec (initial attitude);
1 min (full alignment)
Heading range
+/- 180°
Attitude accuracy
0.3° (1 sigma)>
Altitude accuracy
45 ft at S.L.,
at 40,000 ft altitude
Altitude range
-1,000 ft to 50,000 ft
GPS antenna power
5 V>
Airspeed accuracy
<2 knots @ 40 knots, >
<1 knot @ 60 knots>
Angle of attack range
+/- 8° at max airspeed
Angle of sideslip range
+/- 8° at max airspeed
Max airspeed
120 knots standard, up to >
650 knots optional
IMU performance
Maximum angular rates
+/- 200°/s
Maximum g range
+/- 8 g
Environmental Specifications
Operating Temperature
-40 to 70 ℃
Non-operating temperature
-54 to 85°C
Operating vibration/shock
MIL-STD-810
Humidity
95%, non-condensing
