| CPC G05D 1/0027 (2013.01) [B64C 37/02 (2013.01); B64C 39/02 (2013.01); B64C 39/04 (2013.01); G05D 1/00 (2013.01); G05D 1/104 (2013.01); B64U 2101/30 (2023.01); B64U 2201/102 (2023.01); B64U 2201/20 (2023.01)] | 16 Claims | 

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               1. A flying surface comprising: 
            a plurality of interconnected flying vehicles each comprising an associated thrust unit and an associated controller, wherein adjacent interconnected flying vehicles of the plurality of interconnected flying vehicles are connected via a joint formed between connectors of the adjacent interconnected flying vehicles; and wherein the controller of each of the plurality of interconnected flying vehicles is configured for distributed flight control of the flying surface, wherein the controllers of the plurality of interconnected flying vehicles are collectively configured to reconfigure a shape of the flying surface during flight, wherein said shape comprises a conical shape and a concave shape. 
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