Title :
Notice of Retraction
Design of dynamic testing system for airscrew electric propulsion systems of stratosphere airship
Author :
Linlin He ; Yanfang Wang ; Wenli Huang
Author_Institution :
Sch. of Mechatron. Eng., Zhengzhou Inst. of Aeronaut. Ind. Manage., Zhengzhou, China
Abstract :
Notice of Retraction
After careful and considered review of the content of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE´s Publication Principles.
We hereby retract the content of this paper. Reasonable effort should be made to remove all past references to this paper.
The presenting author of this paper has the option to appeal this decision by contacting TPII@ieee.org.
For the effective function verifying problem of airscrew electric propulsion systems in the state of flight, based on the structural characteristics and operational principles of the propulsion systems, a design of dynamic testing system is proposed in this paper by analyzing the principle of testing method. The technological scheme, hardware structure and software structure of the testing system are introduced, which provide effective research route and foundation for propulsion systems testing.
Keywords :
aerospace engineering; airships; dynamic testing; electric propulsion; stratosphere; airscrew electric propulsion system; dynamic testing system; function verifying problem; hardware structure; operational principle; software structure; state of flight; stratosphere airship; structural characteristics; Brushless DC motors; Permanent magnet motors; Propellers; Temperature measurement; Airscrew electric propulsion systems; Dynamic test; Stratospheric airship; Testing system;
Conference_Titel :
Computer Application and System Modeling (ICCASM), 2010 International Conference on
Conference_Location :
Taiyuan
Print_ISBN :
978-1-4244-7235-2
DOI :
10.1109/ICCASM.2010.5622278
