NDLI: Aircraft attitude control

Content Provider	Springer Nature Link
Author	Zolotukhin, Yu. N. Nesterov, A. A.
Copyright Year	2015
Abstract	The problem of control of the aircraft attitude in a three-dimensional space is considered. The attitude is described by the Euler angles between the axes of the body-fixed coordinate system and the Earth frame. A method of calculating the torque driving the aircraft to a prescribed attitude is proposed. A controller implementing this method is presented. Results of simulations are reported.
Starting Page	456
Ending Page	461
Page Count	6
File Format	PDF
ISSN	87566990
Journal	Optoelectronics, Instrumentation and Data Processing
Volume Number	51
Issue Number	5
e-ISSN	19347944
Language	English
Publisher	Allerton Press
Publisher Date	2015-12-05
Publisher Place	New York
Access Restriction	One Nation One Subscription (ONOS)
Subject Keyword	aircraft attitude attitude control torque Optics, Optoelectronics, Plasmonics and Optical Devices
Content Type	Text
Resource Type	Article
Subject	Instrumentation Condensed Matter Physics Electrical and Electronic Engineering

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Aircraft attitude control