tailieunhanh - Systematic design of an atmospheric data acquisition flying vehicle telemetry system

In this paper, we have provided hands-on experience in systematic design, implementation and flight test of an atmospheric data acquisition flying vehicle as a standard CanSat telemetry mission. This system is designed for launching from a rocket at a separation altitude about 1000-meter. | Systematic design of an atmospheric data acquisition flying vehicle telemetry system Engineering Solid Mechanics 2 2014 265-276 Contents lists available at GrowingScience Engineering Solid Mechanics homepage esm Systematic design of an atmospheric data acquisition flying vehicle telemetry system Vahid Bohlouria Amir Reza Kosaria and MRM Alihab a Faculty of New Science and Technology University of Tehran Iran b Welding and Joining Research Center School of Industrial Engineering Iran University of Science and Technology IUST Narmak 16846-13114 Tehran Iran ARTICLE INFO ABSTRACT Article history In this paper we have provided hands-on experience in systematic design implementation and Received March 6 2014 flight test of an atmospheric data acquisition flying vehicle as a standard CanSat telemetry Accepted 23 August 2014 mission. This system is designed for launching from a rocket at a separation altitude about Available online 1000-meter. During its flight the reusable flying vehicle collects environmental data and 24 August 2014 Keywords transmits it directly to the ground station. The ground station which is implemented at a pre- Flying Vehicle defined radio frequency band receives data and plots the respective graphs. The design CanSat performs based on a systematic approach in which the first step is set aside to mission and Systematic Design objectives definition. In the next step the system requirements are identified and the required Telemetry System main subsystems and elements with their technical requirements will be extracted. The structure analyses were also performed by ABAQUS software to obtain the natural frequency and the mode shape. The wireless communications onboard microcontroller programming sensor interfacing and analog to digital conversion describe the basic technologies employed in the system implementation. This flying vehicle in comparison with the other similar ones is more lightweight has few interface circuits and