A STUDY OF UNMANNED GLIDER DESIGN, SIMULATION, AND MANUFACTURING
This paper describes a mini unmanned glider's design, simulation, and manufacturing with a wing-folding mechanism. The mini-glider is designed for the CANSAT 2016 competition, which has the theme of a Mars glider concept with atmosphere data acquisition. The aim is to facilitate transportation and to land it to the destination point. Having a light and compact design is important since it is a glider without an engine and it uses power only for the transmission of sensory data. The glider is produced with a wingspan which is 440 mm, and its longitudinal distance is 304 mm. The wings can be packaged in a fixed size container whose dimensions are 125 mm in diameter and 310 mm in height. The glider's weight is only 144 gr, and it can increase up to 500 gr with maximum with payload. The mechanism, which includes springs and neodymium magnets for wing-folding, is capable of being ready in 98 ms for gliding after separation from its container. The mini-glider is capable of telemetry, communications, and other sensory operations autonomously during flight.
Bachuta, M. J., et al. "UAV glider control system based on dynamic contraction method." Methods and Models in Automation and Robotics (MMAR), 2012 17th International Conference on. IEEE, 2012.
Beeler, Scott C., Daniel D. Moerder, and David E. Cox. "A flight dynamics model for a small glider in ambient winds." (2003).
Chauffaut, Corentin, Juan Escareno, and Rogelio Lozano. "The transition phase of a gun-launched micro air vehicle." Journal of Intelligent & Robotic Systems70.1-4 (2013): 119-131.
Dilão, Rui, and João Fonseca. "Dynamic trajectory control of gliders." Advances in Aerospace Guidance, Navigation and Control. Springer Berlin Heidelberg, 2013. 373-386.
Etkin, Bernard, and Lloyd Duff Reid. “Dynamics of flight: stability and control.” Vol. 3. New York: Wiley, 1996.
Felton, S., Tolley, M., Demaine, E., Rus, D., & Wood, R. (2014). A method for building self-folding machines. Science, 345(6197), 644-646.
Gao, Ru-Shan, et al. "A Novel Approach to Atmospheric Measurements Using Gliding UASs." Dynamic Data-Driven Environmental Systems Science. Springer International Publishing, 2015. 10-15.
Garza, Frederico R., and Eugene A. Morelli. "A collection of nonlinear aircraft simulations in Matlab." (2003).
Koehl, Arnaud, et al. "Aerodynamic modelling and experimental identification of a coaxial-rotor UAV." Journal of Intelligent & Robotic Systems 68.1 (2012): 53-68.
Kräuchi, Andreas, and Rolf Philipona. "Return glider radiosonde for in situ upper-air research measurements." Atmospheric Measurement Techniques 9.6 (2016): 2535-2544.
Landon, Steven D. "Development of deployable wings for small unmanned aerial vehicles using compliant mechanisms."
Mueller, Thomas J. “Fixed and flapping wing aerodynamics for micro air vehicle applications.” Vol. 195. AIAA, 2001.
Smith, Andrew J. "Aerial Deployed Unfolding Autonomous Glider System." 53rd AIAA Aerospace Sciences Meeting. 2015.
U. S. Navy, "Sonobuoy Tube-launched UAV," STTR, Ed., 2004.
Yechout, Thomas R. Introduction to aircraft flight mechanics. Aiaa, 2003.
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