DocumentCode :
133127
Title :
MIMO closed-loop subspace model identification and hovering control of a 6-DOF coaxial miniature helicopter
Author :
Kojio, Jyunki ; Ishibashi, Haruka ; Inoue, Ryo ; Ushida, Shun ; Oku, Hideki
Author_Institution :
Osaka Inst. of Technol., Osaka, Japan
fYear :
2014
fDate :
9-12 Sept. 2014
Firstpage :
1679
Lastpage :
1684
Abstract :
This paper concerns black-box modeling of a radio-controlled (RC) coxial miniature helicopter by closed-loop subspace model identification with a multi-input and multi-output (MIMO) state space model, as well as model-based control design of hovering flight using the identified black-box model. The RC helicopter has 6 degrees of freedom (6-DOF) in its motions, namely, the lateral (left/right), vertical (up/down), longitudinal (fore/aft), pitching, rolling and yawing axes. These 6 parameters of the position and posture, as the outputs of the RC helicopter, are measured by a motion capture system with 6 high-speed cameras. The helicopter maneuvers, as the inputs, are done by the aileron, elevator, rudder and throttle. A closed-loop system identification experiment of the hovering RC helicopter is performed. CL-MOESP, which is one of closed-loop subspace model identification methods, is applied to the sampled closed-loop data in order to obtain a state-space model with an estimated order. Using the identified model, an LQ controller with a full-state observer is designed. Finally, as verification of the identified model, an experiment of hovering flight of the helicopter is performed with the implementation of the feedback controller.
Keywords :
MIMO systems; aircraft control; closed loop systems; control system synthesis; feedback; helicopters; 6-DOF coaxial miniature helicopter; MIMO closed-loop subspace model identification; closed-loop system; feedback controller; hovering control; hovering flight; model-based control design; multiinput and multioutput state space model; radio-controlled coxial miniature helicopter; Adaptive control; Control design; Helicopters; MIMO; Mathematical model; Observers; Position measurement; autonomous flight control; closed-loop identification; miniture helicopter; subspace method; system identification experiment;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
SICE Annual Conference (SICE), 2014 Proceedings of the
Conference_Location :
Sapporo
Type :
conf
DOI :
10.1109/SICE.2014.6935291
Filename :
6935291
Link To Document :
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