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專利授權區

專利授權區
專利名稱(中)	雙自旋雷射無人機導引降落系統及方法
專利名稱(英)	DUAL SPINNING LASER-BASED UAV POSITIONING AND LANDING SYSTEM AND METHOD
專利家族	中華民國：I893999 大陸：CN121734723A(公開號) 美國：(公開號)
專利權人	國立清華大學 100.00%
發明人	許健平,郭永清
技術領域	資訊工程,機械結構

專利摘要(中)
一種雙自旋雷射無人機導引降落系統，包括第一雷射模組、第一旋轉模組、第二雷射模組、第二旋轉模組、訊號收發器、控制器以及基板。第一雷射模組用以提供繞第一軸旋轉發出的第一光束。第一旋轉模組用以帶動第一雷射模組繞垂直於第一軸的旋轉軸旋轉，使第一光束在空間中掃描。第二雷射模組用以提供繞第二軸旋轉發出的第二光束。第二旋轉模組用以帶動第二雷射模組繞垂直於第二軸的旋轉軸旋轉，使第二光束在空間中掃描。在第一光束先投射在無人機上時，無人機發出訊號。在訊號收發器接收訊號後，控制器取得第一夾角。在第二光束再投射在無人機上時，無人機發出訊號。在訊號收發器接收訊號後，控制器取得第二夾角且計算相對位置，並控制訊號收發器將相對位置訊號傳送至無人機。一種雙自旋雷射無人機導引降落方法亦被提出。

專利摘要(中)

一種雙自旋雷射無人機導引降落系統，包括第一雷射模組、第一旋轉模組、第二雷射模組、第二旋轉模組、訊號收發器、控制器以及基板。第一雷射模組用以提供繞第一軸旋轉發出的第一光束。第一旋轉模組用以帶動第一雷射模組繞垂直於第一軸的旋轉軸旋轉，使第一光束在空間中掃描。第二雷射模組用以提供繞第二軸旋轉發出的第二光束。第二旋轉模組用以帶動第二雷射模組繞垂直於第二軸的旋轉軸旋轉，使第二光束在空間中掃描。在第一光束先投射在無人機上時，無人機發出訊號。在訊號收發器接收訊號後，控制器取得第一夾角。在第二光束再投射在無人機上時，無人機發出訊號。在訊號收發器接收訊號後，控制器取得第二夾角且計算相對位置，並控制訊號收發器將相對位置訊號傳送至無人機。一種雙自旋雷射無人機導引降落方法亦被提出。

專利摘要(英)
A dual spinning laser-based UAV positioning and landing system includes a first laser module, a first rotation module, a second laser module, a second rotation module, a signal transceiver, a controller and a substrate. The first laser module is configured to provide a first beam emitted by rotating around a first axis. The first rotation module is configured to drive the first laser module to rotate around a rotation axis perpendicular to the first axis, so that the first beam scans in a space. The second laser module is configured to provide a second beam emitted by rotating around a second axis. The second rotation module is configured to drive the second laser module to rotate around a rotation axis perpendicular to the second axis, so that the second beam scans in the space. When the first beam is first projected on a UAV, the UAV emits a signal. After the signal transceiver receives the signal, the controller obtains a first included angle. When the second beam is then projected on the UAV, the UAV emits the signal. After the signal transceiver receives the signal, the controller obtains a second included angle and calculates a relative position, and controls the signal transceiver to transmit a relative position signal to the UAV. A dual spinning laser-based UAV positioning and landing method is also provided.

專利摘要(英)

A dual spinning laser-based UAV positioning and landing system includes a first laser module, a first rotation module, a second laser module, a second rotation module, a signal transceiver, a controller and a substrate. The first laser module is configured to provide a first beam emitted by rotating around a first axis. The first rotation module is configured to drive the first laser module to rotate around a rotation axis perpendicular to the first axis, so that the first beam scans in a space. The second laser module is configured to provide a second beam emitted by rotating around a second axis. The second rotation module is configured to drive the second laser module to rotate around a rotation axis perpendicular to the second axis, so that the second beam scans in the space. When the first beam is first projected on a UAV, the UAV emits a signal. After the signal transceiver receives the signal, the controller obtains a first included angle. When the second beam is then projected on the UAV, the UAV emits the signal. After the signal transceiver receives the signal, the controller obtains a second included angle and calculates a relative position, and controls the signal transceiver to transmit a relative position signal to the UAV. A dual spinning laser-based UAV positioning and landing method is also provided.

聯絡資訊
承辦人姓名	李曉琪
承辦人電話	03-5715131 #31061
承辦人Email	hsiaochi@mx.nthu.edu.tw