TY - GEN
T1 - Hardware-in-the-loop (Hil) and experimental findings for the 7 kw pumping kite power system
AU - Dief, Tarek N.
AU - Rushdi, Mostafa A.
AU - Halawa, Amr M.
AU - Yoshida, Shigeo
N1 - Publisher Copyright:
© 2020, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2020
Y1 - 2020
N2 - This paper presents the experimental work of airborne wind energy, kite system, as a power source, developed in Kyushu University. Kite extracts more energy from high altitude wind with less foundations compared with the wind turbines. This paper demonstrates the 7kW kite system of Kyushu University including the system’s design, tests, and experimental results. The kite system consists of inflatable wing with fixed tether length. The kite is controlled by small device, kite control unit (KCU), as a hardware-in the loop (HIL). This technique is utilized to develop and perform the real-time flight test of the kite. It provides an effective algorithm by adding the complexity of the system under control. Several tests had been performed to analyse the kite performance, and tension forces result from those tests are presented in different truck speeds and flight cases.
AB - This paper presents the experimental work of airborne wind energy, kite system, as a power source, developed in Kyushu University. Kite extracts more energy from high altitude wind with less foundations compared with the wind turbines. This paper demonstrates the 7kW kite system of Kyushu University including the system’s design, tests, and experimental results. The kite system consists of inflatable wing with fixed tether length. The kite is controlled by small device, kite control unit (KCU), as a hardware-in the loop (HIL). This technique is utilized to develop and perform the real-time flight test of the kite. It provides an effective algorithm by adding the complexity of the system under control. Several tests had been performed to analyse the kite performance, and tension forces result from those tests are presented in different truck speeds and flight cases.
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U2 - 10.2514/6.2020-1244
DO - 10.2514/6.2020-1244
M3 - Conference contribution
AN - SCOPUS:85085161727
SN - 9781624105951
T3 - AIAA Scitech 2020 Forum
BT - AIAA Scitech 2020 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Scitech Forum, 2020
Y2 - 6 January 2020 through 10 January 2020
ER -