An Automatic Flight Control Requirement
Envisaged to provide navigation and inertial parameters to avionics systems on airborne platforms
Consists of integrated inertial sensors (Gyros and Accelerometers) and GNSS receiver to provide the parameters like Angular and linear accelerations, Angular Rates, Linear Velocity, Present Position and Altitude, Attitude and Heading, Roll, Pitch and Azimuth, Magnetic Heading
The invisible pieces of technology that people rely on everyday
Preferably based on low-cost sensors which can meet adequate navigation accuracy. Perform automatic alignment. Capable of determining accelerations, velocity, position, body rates, attitude and heading to the accuracies specified herein in the pure inertial mode from take-off to landing after alignment.