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Laboratory Testing for ITB HALE-UAV Control System
Abstract
High Altitude and Long Endurance (HALE) UAV is the one of CentrUMS-ITB UAV that has been developing on progress. There are some important aspect behind the HALE technology Development process, one of them is the control system. This paper will describe the hardware configuration design of HALE ITB-UAV and also the laboratory testing setup to support the development process of them. On the target flight condition there are some critical environment especially temperature, and low pressure. So there are several requirement that must be owned by the control system to make this system will work properly. Step by step design consideration and also the testing method will be described on this paper.
References
Manish R. Bhatt, “Solar Power Unmanned Aerial Vehicle : High Altitude and Long Endurance Application (HALE
SPUAV)”, Project Report, Department of Mechanical and Aerospace Engineering, San Jose State of University, May,
, Craight L. Nickol, Mark D. Guynn, Lisa L. Kohout, Thomas A. Ozorosky, “High Altitude and Long Endurance UAV
Analysis of alternatives Technology Requirements Development”, NASA TP-2007-214861, 2007
Mustafa cavcar, “The International standard Atmosphere (ISA), School of Civil Aviation, Anadolu Univeristy, 26470
Eskisehir , Turkey.
DOI: http://dx.doi.org/10.21535%2FProICIUS.2013.v9.208
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