Vision based aircraft cabin ambient light control
A vision-based aircraft cabin light monitoring/control system is used to maintain the light intensity level within the aircraft cabin at a desired level. The system uses video cameras to continuously monitor the ambient light entering the passenger cabin windows, analyzes the video stream/feed to identify the light intensity level within the cabin, identifies the window whose state should be controlled, and generates commands to control the window through central cabin controllers. The system further compensates for light sources internal to the cabin and monitors the phase of flight to ensure compliance to specific light conditions within the aircraft cabin.
1 . An aircraft cabin ambient light control system for monitoring and controlling the light intensity level within an aircraft cabin, the system comprising:
a dimmable window having an electrically controllable opacity level;
a central cabin controller electrically coupled to the dimmable window;
and an ambient light controller electrically coupled to the central cabin controller, wherein the ambient light controller comprises a processing unit electrically coupled to a plurality of cameras and a communication interface, and wherein:
the plurality of cameras continuously capture video within the aircraft cabin and transfer the video stream to the processing unit;
the processing unit analyzes the video and identifies a light intensity level within the aircraft cabin;
the communication interface sends data to the electrically coupled central cabin controller;
the central cabin controller sends a command signal to the dimmable window to control the opacity level of the dimmable window;
wherein the processing unit comprises:
a video capture module configured to capture the video from the plurality of cameras;
a video analyzer module configured to process the video from the plurality of cameras to remedy low light and low-resolution videos;
a light intensity level identifier module configured to analyze the processed video from the plurality of cameras to identify the light intensity level within the aircraft cabin; and
a window locator module configured to analyze features extracted from the processed video to identify dimmable windows which require an opacity level adjustment.
2 . The system of claim 1 and further comprising a local window controller electrically coupled to and positioned between the dimmable window and the central cabin controller, wherein the local window controller receives the command signal from the central cabin controller, and wherein the local window controller controls the opacity level of the dimmable window.
3 . The system of claim 2 , wherein:
the aircraft includes a plurality of dimmable windows;
each of the plurality of dimmable windows are electrically coupled to a single local window controller; and
each of the local window controllers are positioned between and electrically coupled to the central cabin controller and one of the plurality of dimmable windows.
4 . The system of claim 1 and further comprising a crew access panel electrically coupled to the central cabin controller, wherein an aircraft crew member interacts with the crew access panel to manually control the opacity level of the dimmable window.
5 . The system of claim 4 , wherein the aircraft crew member interacts with the crew access panel to allow or prevent an aircraft passenger from controlling the opacity level of the dimmable window.
6 . The system of claim 1 , wherein the ambient light controller transfers data through the communication interface to the central cabin controller to automatically control and adjust the dimmable window opacity level based on phase of flight data received from an avionics system within the aircraft.
7 . The system of claim 6 , wherein the ambient light controller adjusts the dimmable window to a low opacity level during takeoff and landing of the aircraft, and wherein the ambient light controller adjusts the dimmable window to a high opacity level during cruise phase of flight.
8 . The system of claim 1 , wherein the ambient light controller is configured to detect and locate a fire within the aircraft cabin, and wherein the ambient light controller transfers a warning signal through the communication interface to the central cabin controller indicating that a fire has been detected and located within the aircraft cabin.
9 . The system of claim 8 , wherein the ambient light controller detects a fire within the aircraft cabin by comparing and identifying that the light intensity level within the aircraft cabin has exceeded a predefined fire threshold light intensity value.