AUTOPILOT SYSTEMS

Autopilot Systems

  • Indigenous design and developed

  • Fully digital autopilot

  • Onboard 10 Degree of Freedom (DoF) IMU Onboard  3 Axes Sensors (Gyro, Accelerometer, Magnetometer)  + Altitude

  • External Reconfigurable Interface (for GPS, Sonar, Airspeed Sensor, Gas Sensor, RF System etc.)

  • 8 to 16 Channel PWM Interfaces

  • Input Voltage : + 5 to +12 V

  • Tested on 5 different platform

  • > 250 Flight test completed

  • Flown in various flight modes (like Manual, Stabilize, FBW-A, FBW-B, Auto, Waypoints Navigation etc.)

  • Onboard (Flash or microSD) flight data logger

  • 2 to 6 Hours flight data log for more than 100 parameters

  • Weight = 4.2 to 12.3 grams

  • Dimension = (30 x 25) mm to    (50 x 50) mm

 

FLIGHT TEST PERFORMANCE

TECHNICAL SPECIFICATIONS

 

Parameter

Description

Range

Processor

ARM CortexM3 CPU core

32 - Bits

Power

Input Voltage

1.8 - 3.3 Volt

I2C

2 I2C Port

100/400 Kbps

UART

3 UART Port

9.6/57.6 Kbps

SPI

2 SPI Port

>1 Mbps

PWM

16-Channel PWM

3.3 V

Temperature

Industrial temperature

-40 to +85°C

Onboard Sensors

3 Axes (Gyro, Accelerometer, Magnetometer) + Static Pressure

As per sensors

External Reconfigurable Interface

GPS, Sonar, Airspeed Sensor, Gas Sensor, RF System, Control Servos

Deg C

Flight Modes

Manual, Stabilize, FBW-A, FBW-B, Auto, Waypoints Navigation

Tested in All Flight Modes

Flight Test

>250 Flight Test Conducted

Tested on Five Different Platform

Last updated on : 09-11-2020 11:26:17am