| CPC B64D 11/0606 (2014.12) [B64D 11/0602 (2014.12); B64D 11/0626 (2014.12); A61B 5/6888 (2013.01); H04L 12/2816 (2013.01); Y04S 20/20 (2013.01)] | 17 Claims | 

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               14. An aircraft passenger suite comprising: 
            an aircraft seat for use by a passenger; and 
                a controller for controlling a number of output states of the aircraft passenger suite, the controller comprising: 
                a first receiver operable to receive a logic condition input; and 
                  a second receiver operable to receive image, pressure and/or physiological sensor data from sensor equipment, the sensor data representing a three-dimensional thermal map of a volume within the aircraft passenger suite and providing an indication of one or more attributes of a passenger of the aircraft passenger suite, 
                wherein the controller is configured to control at least one of the output states of the aircraft passenger suite based on both the logic condition input and the sensor data. 
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