| CPC G01S 7/51 (2013.01) [B64D 47/00 (2013.01); B64U 10/14 (2023.01); G01S 7/4813 (2013.01); G01S 17/42 (2013.01); G01S 17/89 (2013.01); G05D 1/0094 (2013.01); G05D 1/101 (2013.01); G06F 3/04845 (2013.01); G06T 15/00 (2013.01); G06T 15/08 (2013.01); B64U 2101/30 (2023.01); G06T 2200/24 (2013.01); G06T 2210/56 (2013.01)] | 18 Claims | 

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               1. A movable object, comprising: 
              a propulsion system; 
                a main body coupled to the propulsion system; 
                a payload assembly coupled to the main body via a payload port, the payload assembly comprising a payload support bracket configured to couple to the payload port and support a scanning sensor; 
                a positioning sensor; 
                at least one memory including instructions; and 
                at least one processor, wherein the instructions when executed by the at least one processor, cause the movable object to at least to: 
                receive control data from an external device, 
                  move the scanning sensor with respect to the movable object via a movement of the payload assembly based on the control data, 
                  obtain mapping data from the scanning sensor in a first coordinate system based on the control data, 
                  obtain positioning data from the positioning sensor, 
                  construct a dense map in real-time based on the mapping data and the positioning data, and 
                  transform the dense map into a sparse map; 
                and 
                a communication device configured to transmit the sparse map to the external device in real-time 
              wherein the external device is configured to: 
            receive the sparse map; and 
                render the sparse map in a second coordinate system in real-time, the second coordinate system being different from the first coordinate system, 
                wherein the first coordinate system is a scanner reference coordinate system, and the second coordinate system is a north-east-down (NED) coordinate system or a FlightGear coordinate system. 
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