发明名称 ROTARY WING AIRCRAFT FLIGHT CONTROL SYSTEM WITH A PROXIMITY CUEING AND AVOIDANCE SYSTEM
摘要 An obstacle avoidance system according to the present invention may include an input control device, a sensor suite, and a communication feedback loop. The input control device is preferably operable to create a first force, while the sensor suite is configured to detect nearby obstacles, and the communication feedback loop is in communication with the input control device and the senor suite so that said communication feedback loop is operable to generate a command signal in response to detection of a nearby obstacle. The command signal being operable to cause an actuator to generate a second force different from said first force. Preferably, the obstacle avoidance system is used in combination with an apparatus, such as a rotary wing aircraft, wherein the input control device at least partially controls the movement of the apparatus in response to a user's input. The user's input tending to cause the first force to move the apparatus in a first direction. The sensor suite being preferably mounted to the apparatus in order to detect nearby obstacles which may contact the apparatus if the apparatus is moved in the first direction. The communication feedback loop at least partially augmenting the user's input such that the second force tends to preclude the apparatus from moving in the first direction and thus tends to preclude the apparatus from contacting the detected obstacle. More preferably, the second force tends to cause the apparatus to move in a second direction different from the first direction and away from the detected obstacle.
申请公布号 WO2007024635(A2) 申请公布日期 2007.03.01
申请号 WO2006US32215 申请日期 2006.08.17
申请人 SIKORSKY AIRCRAFT CORPORATION 发明人 MATUSKA, DAVID, G.;SAHASRABUDHE, VINEET;ANTTILA, DONALD, S.
分类号 G01C5/00;G08G1/16 主分类号 G01C5/00
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