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