TY - GEN
T1 - Blade-tip close warning situational awareness laser system for improving helicopter safety
AU - Zhang, Lei
AU - Zhou, Yaoming
AU - Wu, Zhe
PY - 2011
Y1 - 2011
N2 - In order to improve the helicopter operation safety in complex terrain or brown-out environments, a Blade-Tip close warning situation awareness Laser System (BTLS) with the detection range of 360-degree circumferential directions and the height direction to improve the helicopter situational awareness ability is proposed. The BTLS consists of blade-tip orthogonal laser transmitters, fuselage laser receiver array, and the laser drive controller, in which the transmitters, receivers, and fiber optic connections are all redundant. The most important feature of the BTLS is the two orthogonal directions of the transmitters installed in the blade-tip, using the helicopter itself rotating parts - blades to achieve quick scan of 360-degree circumferential directions and the height direction, thus overcoming the disadvantages of existing laser detectors of complex scan mechanism, lack detection range and installation location restrictions. The effects of the three angles of the helicopter blade in normal flight states and the helicopter pitch angle in high speed forward flight state on the BTLS performance are analyzed. The results showed that the BTLS has less 4% relative error whatever in circumferential directions or in height direction at the normal flight states except at the high speed forward flight state, there was a blind area in front. The BTLS is light weight, low power consumption, wide detection range, flexible installation location, high reliability, having high research value and good prospects.
AB - In order to improve the helicopter operation safety in complex terrain or brown-out environments, a Blade-Tip close warning situation awareness Laser System (BTLS) with the detection range of 360-degree circumferential directions and the height direction to improve the helicopter situational awareness ability is proposed. The BTLS consists of blade-tip orthogonal laser transmitters, fuselage laser receiver array, and the laser drive controller, in which the transmitters, receivers, and fiber optic connections are all redundant. The most important feature of the BTLS is the two orthogonal directions of the transmitters installed in the blade-tip, using the helicopter itself rotating parts - blades to achieve quick scan of 360-degree circumferential directions and the height direction, thus overcoming the disadvantages of existing laser detectors of complex scan mechanism, lack detection range and installation location restrictions. The effects of the three angles of the helicopter blade in normal flight states and the helicopter pitch angle in high speed forward flight state on the BTLS performance are analyzed. The results showed that the BTLS has less 4% relative error whatever in circumferential directions or in height direction at the normal flight states except at the high speed forward flight state, there was a blind area in front. The BTLS is light weight, low power consumption, wide detection range, flexible installation location, high reliability, having high research value and good prospects.
UR - https://www.scopus.com/pages/publications/84255194357
U2 - 10.1109/DASC.2011.6096147
DO - 10.1109/DASC.2011.6096147
M3 - 会议稿件
AN - SCOPUS:84255194357
SN - 9781612847979
T3 - AIAA/IEEE Digital Avionics Systems Conference - Proceedings
SP - 8C41-8C48
BT - 30th Digital Avionics Systems Conference - Closing the Generation Gap
T2 - 30th Digital Avionics Systems Conference - Closing the Generation Gap: Increasing Capability for Flight Operations among Legacy, Modern and Uninhabited Aircraft, DASC 2011
Y2 - 16 October 2011 through 20 October 2011
ER -