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This paper proposes an autopilot system that can be used to control the smallscale rotorcraft during the flight test for linear-frequency-domain systemidentification. The input frequency swept is generated automatically as part ofthe autopilot control command. Therefore the bandwidth coverage and consistencyof the frequency swept is guaranteed to produce high quality data for systemidentification. Beside that we can set the safety parameter during the flighttest (maximum roll or pitch value, minimum altitude, etc) so the safety of thewhole flight test is guaranteed. This autopilot for automated flight test willbe tested using hardware in the loop simulator for hover flight condition.

Automated Flight Test and System Identification for Rotary Wing Small Aerial Platform using Frequency Responses Analysis