Thor Flight 25

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https://hdl.handle.net/11299/174304

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Title

Thor Flight 25

Authors

Taylor, Brian

Published Date

2011-10-05

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Abstract

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Thor Flight

ACRC

Anoka

Control

System Identification

Multisine

Description

The controller used for flight 23 was the baseline controller. For 24 and 25 it was the composite student controller, with the following gains: pitch_gain[3] ={-0.6, -0.09, 0.08}; group 1, v1 roll_gain[3]={-0.45, -0.022, 0.05}; group 3, v1 Software used was /branches/flightcode_nav/ rev 643 for flight 23, rev 645 for flights 24 and 25. Thor Flight 25: student controller, system id multisine input on the rudder. Straight and level for 3 seconds, then hold elevator and inject a 15 second multisine that covers 0.2 to 3.0 Hz, amplitude 3 deg. Lateral-directional controller still engaged. Onboard video and motor data collected. R/C Rx: A=21,L=0,F=0,H=0.

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Taylor, Brian. (2011). Thor Flight 25. Retrieved from the University Digital Conservancy, https://hdl.handle.net/11299/174304.

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