Patent classifications
B64D45/0056
VEHICLE OPERATOR MONITORING SYSTEM WITH SMART ACTIVE ENGAGEMENT AND DISENGAGEMENT
An operator safety system (OSS) monitors the physiological well-being of an aircraft pilot or vehicle operator, and has engaged and disengaged operational states (the engaged state associated with active monitoring). The OSS includes a smart engage/disengage system incorporating presence sensors (e.g., visual, seat-based) installed in the cockpit or control area of the vehicle. When the presence sensors determine that the pilot/operator is no longer present in their seat but the OSS is still engaged, the OSS prompts the operator to disengage the OSS (e.g., via single-touch display interface or remotely to a mobile device). When the presence sensors determine that the operator is present or seated, but the OSS is disengaged, the OSS prompts the operator to re-engage the OSS.
Approach mode activation monitoring function and automatic activation in an event of pilot incapacitation
Aircraft systems and methods that determine, based on location data from a navigation system, whether conditions have been met enabling arming of an approach mode of an autopilot system. The systems and methods, when the one or more conditions enabling arming of the approach mode are determined to be met, start a first timer of a first period of time and, at the same time, provide a first message to alert a pilot to arm the approach mode via manual input to a user interface. When a determination has been made that the approach mode continues to have not been armed via manual input to the user interface, the approach mode is automatically armed.
Emergency control of an aircraft
An aircraft emergency control system comprises at least one sensor configured to output an electronic signal relating to detection of incapacitation of at least one aircraft crew member. A processor is configured to receive and process the electronic signal to determine whether emergency action is to be taken. A control unit is configured to communicate, in use, a control signal to an avionics system of the aircraft in relation to the emergency action if the processor determines that emergency action is to be taken.
METHODS AND SYSTEMS FOR CONTROLLED DISEMBARKATION OF AIRCRAFT PASSENGERS
A passenger aircraft includes a plurality of passenger seats arranged in seat rows, and a disembarkation guidance system. The disembarkation guidance system includes a plurality of electronically operable visual indicators, each of the plurality of electronically operable visual indicators being assigned to a respective seat row. The disembarkation guidance system further includes an indicator control device coupled to each of the electronically operable visual indicators. The indicator control device is configured to individually control electronically operable visual indicators to indicate passengers in the assigned seat row whether they are permitted to disembark the passenger aircraft.
Object monitoring system for aircraft
A method, apparatus, system, and computer program product for monitoring a platform. Images are received by a computer system from a sensor system positioned to monitor movement of human beings relative to the platform. A set of the human beings is identified by the computer system in the images. The movement of the set of the human beings relative to the platform is determined by the computer system using the images. A count of the human beings on the platform is determined by the computer system based on the movement determined for the set of the human beings. A set of actions is performed by the computer system based on the count of the human beings on the platform.
Monitoring device and method for monitoring a movement profile of a user in the region of an actuating element of an aircraft or spacecraft
A monitoring device for monitoring a movement profile of a user in the region of an actuating element of an aircraft or spacecraft, having at least one movement sensor which is configured to detect a first monitoring space of the monitoring device and at the same time a second monitoring space of the monitoring device which differs from the first monitoring space. Also a method for monitoring a movement profile of a user in the region of an actuating element of an aircraft or spacecraft, with: detection of a first monitoring space of the monitoring device by at least one movement sensor; and simultaneous detection of a second monitoring space, which is different from the first monitoring space, by the at least one movement sensor.
Object Monitoring System for Aircraft
A method, apparatus, system, and computer program product for monitoring a platform. Images are received by a computer system from a sensor system positioned to monitor movement of human beings relative to the platform. A set of the human beings is identified by the computer system in the images. The movement of the set of the human beings relative to the platform is determined by the computer system using the images. A count of the human beings on the platform is determined by the computer system based on the movement determined for the set of the human beings. A set of actions is performed by the computer system based on the count of the human beings on the platform.
AIRCRAFT PASSENGER SERVICE UNIT HEALTH MONITORING SYSTEM
A passenger service unit health monitoring system includes a cardiorespiratory sensor unit, a temperature sensor, and one or more controllers having one or more processors configured to execute a set of program instructions maintained in one or more memory units, wherein the set of program instructions is configured to cause the one or more processors to: receive one or more signals from at least one of the temperature sensor or the cardiorespiratory sensor unit indicative of one or more physiological states of the subject; measure one or more physiological states of the subject based on the one or more signals indicative of one or more physiological states of the subject; determine one or more physiological interventions based on the one or more physiological states of the subject; and transmit one or more signals instructive of the one or more physiological interventions.
SYSTEM AND METHOD FOR MEASURING WEIGHT AND BALANCE ON AN AIRCRAFT
A system for calculating weight and distribution on an aircraft. The system includes an aircraft, at least one cabin camera configured to view the cabin of the aircraft, an image collector configured to collect images from the at least one cabin camera and a processor. The processor is configured to perform the following steps: a) detecting passengers and/or hand baggage from the images collected from the image collector, b) estimating positions of the passengers and/or hand baggage from the images collected from the image collector, and c) estimating weight of the passengers and/or hand baggage from the images collected from the image collector. The processor also calculates a real-time weight distribution of the aircraft based on the estimates provided in steps a)-c).
DATA-DRIVEN MANAGEMENT SYSTEM AND METHOD FOR PASSENGER SAFETY, HEALTH AND COMFORT
A management system (100) for passenger safety, health and comfort, the system comprising a first module (101) configured to collect data from an array of sensors within a passenger cabin, a first set of parameters based on the data collected by the first module, a second set of parameters based on the data collected by the first module, a second module (120) comprising a processor configured to process the first set of parameters and the second set of parameters. The processor is further configured to determine if passenger comfort levels are in the negative and/or if a passenger is showing symptoms of sickness, determine alterations and/or actions to be taken by an environmental control system and/or crew of the passenger cabin to assist in moving the comfort levels to a positive and/or to assist a sick passenger, and alert the crew and/or alter the environmental control system.