Experimental data

This section is a repository of data suitable for identification purposes. All the files are matlab files (.mat) and contain the following variables: throttle, pedals, longCyclic, latCyclic, x, y, z, pitch, yaw, roll, time. The first 4 variables (throttle, pedals, longCyclic, latCyclic) correspond to the inputs applied to the helicopter through the RC transmitter. The following 6 variables correspond to the position (x, y, z) and attitude (pitch, yaw, roll) of the aircraft. time variable is self-explanatory.

Yaw experiments

• Open loop steps. The other inputs are manually controlled to maintain the helicopter near hover. Data file
• Open loop PRBS + multisinus signal (duration:17s+9.5s, freq. band:0-12Hz). The other inputs are manually controlled to maintain the helicopter near hover. Data file
• Open loop PRBS signal (duration:17s, freq. band:0-12Hz). The other inputs are manually controlled to maintain the helicopter near hover. Data file
• Open loop mulitsinus signal (duration:9.5s, freq. band:0-12Hz). The other inputs are manually controlled to maintain the helicopter near hover. Data file

Altitude experiments

• Open loop steps. The other inputs are manually controlled to maintain the helicopter near hover. Data file
• Open loop PRBS signal (duration:10s, freq. band:). The other inputs are manually controlled to maintain the helicopter near hover. Data file
• Open loop PRBS signal (duration:10s, freq. band:). The other inputs are manually controlled to maintain the helicopter near hover. Data file
• Open loop PRBS signal (duration:10s, freq. band:). The other inputs are manually controlled to maintain the helicopter near hover. Data file

Go back