Notice of RetractionDynamic simulation on retractionextension system of an aircraft

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.

This paper provides a detailed discussion on the simulation of a landing gear retraction /extension(R/E) system. Section 2 of the full paper presents a general description of the R/E system and its retraction procedure. A mathematical model of the R/E system is introduced by Section 3, which gives a basic idea for numerically modeling this mechanism. Section 4 brings up the procedures for constructing the simulation model in LMS Virtual. Lab Motion and Imagine.Lab AMEsim. After analyzing the simulation results of the kinematics and the hydraulic and pneumatic features in section 5, we draw the conclusion that the R/E system design satisfies the requirements imposed by AFSC DH2-1, and measures should be taken to minimize its internal impact.