发明名称 INDOOR MONITORING SYSTEM AND METHOD THEREOF
摘要 An indoor monitoring system and a method thereof are provided. The system includes an aircraft body; an image capturing unit capturing multiple images in an indoor space in an order of a capturing sequence; a storage unit storing a 3D indoor map corresponding to the indoor space, where the 3D indoor map includes multiple default images and a default flying path; a positioning unit generating 3D space information of the aircraft body; a transmitting unit receiving a control instruction or transmit each image; a processing unit driving the aircraft body to fly in the indoor space according to the default flying path and comparing a default image with an image in pairs in the order of the capturing sequence. The position of the aircraft body on the default flying path can be corrected by the comparing result and the goal of monitoring the indoor space can be achieved.
申请公布号 US2016286173(A1) 申请公布日期 2016.09.29
申请号 US201514844814 申请日期 2015.09.03
申请人 Apacer Technology Inc. 发明人 WANG YI-HSIUNG
分类号 H04N7/18;G05D1/08;G06K9/00;B60R1/00;G06K9/62;G05D1/00;B64C39/02 主分类号 H04N7/18
代理机构 代理人
主权项 1. An indoor monitoring method which is applicable to control a micro aircraft in an indoor space, the micro aircraft comprising: an aircraft body, an image capturing unit, a storage unit, a positioning unit, a processing unit, a transmitting unit and a power supply unit, and the method comprising: reading a 3D indoor map stored in the storage unit, wherein the 3D indoor map comprises multiple default images and each default image comprises at least one target; driving the aircraft body to fly in the indoor space according to a default flying path of the indoor map; capturing multiple images in the indoor space in an order of a capturing sequence by the image capturing unit, wherein each captured image comprises at least one feature point; comparing each default image with each captured image in pairs in the order of the capturing sequence; and calculating an offset distance between the aircraft body and the at least one feature point and correcting a position of the aircraft body on the default flying path according to the offset distance when the at least one target of the default image matches the at least one feature point of the captured image in each pair, wherein the processing unit applies 3D space information generated by the positioning unit to further correct the position of the aircraft body on the default flying path.
地址 New Taipei City TW