TY - GEN
T1 - Evaluation of dynamic behavior of a deployable wing UAV by drop test
AU - Fujita, Koji
PY - 2012/12/1
Y1 - 2012/12/1
N2 - Aerial deployment technique is required for next-generation airplanes. In this technique, dynamic behavior of an airplane during deployment motion is one of the critical problems. In order to evaluate this, drop test via a balloon was performed for a small unmanned aerial vehicle (UAV) which has a foldable wing. Flight data and motion were analyzed and it became apparent that symmetric deployment motion by a servo & wire type folding method deployable airplane has no large influence on dynamic behavior.
AB - Aerial deployment technique is required for next-generation airplanes. In this technique, dynamic behavior of an airplane during deployment motion is one of the critical problems. In order to evaluate this, drop test via a balloon was performed for a small unmanned aerial vehicle (UAV) which has a foldable wing. Flight data and motion were analyzed and it became apparent that symmetric deployment motion by a servo & wire type folding method deployable airplane has no large influence on dynamic behavior.
KW - Balloon
KW - Deployable wing
KW - Drop test
KW - Dynamic behavior
KW - UAV
UR - http://www.scopus.com/inward/record.url?scp=84878625189&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=84878625189&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:84878625189
SN - 9781622767540
T3 - 28th Congress of the International Council of the Aeronautical Sciences 2012, ICAS 2012
SP - 1761
EP - 1770
BT - 28th Congress of the International Council of the Aeronautical Sciences 2012, ICAS 2012
T2 - 28th Congress of the International Council of the Aeronautical Sciences 2012, ICAS 2012
Y2 - 23 September 2012 through 28 September 2012
ER -