Abstract: The disclosure reveals a system and approach for remote health monitoring and diagnostics of room controllers, networks and devices. A master room controller may be used to open a system health page or a diagnostic page for other controllers. A system health page may provide an overview of virtually all of the other room controllers. A tool of the present system may be used to trouble shoot issues remotely at another room controller in lieu of doing a visit to the respective room controller. A user may navigate from the system health page to virtually any place on the room controller to diagnose issues. The navigation may be done by hyper linking from the system health page. The healthy controllers may be hidden from the page so that the unhealthy systems can be viewed in one shot.

Abstract: Systems and methods are provided for monitoring aircraft to mitigate potential loss of communication scenarios. One exemplary method involves monitoring a plurality of communications channels using an onboard communications system, maintaining associations between respective communications channel assignments and respective operational contexts based on the plurality of clearance communications, and in response to detecting a change in an operational context of the aircraft, providing indication of a recommended communications channel based on an association between the recommended communications channel and one of the plurality of different operational contexts corresponding to a current operational context of the aircraft.

Abstract: A mask (100), such as a filtration mask, with multiple strap configurations is provided. For example, such mask might be worn in either a head strap (240) or an ear strap (110) configuration. The mask comprises two ear straps each with a connector support element (130) allowing removable attachment of a separate head strap.

Abstract: Devices, methods, and systems for causing a self-testing fire sensing device to initiate a fire response are described herein. One device includes a user interface, a memory, and a processor configured to execute executable instructions stored in the memory to receive, via the user interface, a selection to initiate a fire response, receive, via the user interface, a selection of a self-testing fire sensing device to initiate the fire response, transmit a command to the self-testing fire sensing device to initiate the fire response, and receive a notification of a number of output events triggered by the initiation of the fire response by the self-testing fire sensing device.

Abstract: A system comprises a vehicle radar sensor including an antenna, transmitter, receiver, and processor. The processor hosts a scanning control module that sends a control signal to the transmitter, receiver, or both, to generate radar beams; and a signal processing module that receives a reflected signal from the receiver to generate radar data. The system also includes an onboard application module and ground surface database. The application module is operative to access information from the surface database, access position and attitude data, access position and attitude uncertainty data, access radar installation data, and access radar data from the signal processing module; identify ground surface areas to be avoided based on the information from the surface database, the position and attitude, the position and attitude uncertainty, and the radar installation data; and perform modified radar operations and/or processing when the ground surface areas to be avoided are within a radar FOV.

Abstract: Methods and systems are provided for assisting operation of a vehicle such as an aircraft using a virtual cursor. One method involves identifying a displayed location of an active cursor overlying a first navigational map graphical user interface (GUI) display, determining a geographic reference point on the first navigational map GUI corresponding to the displayed location of the active cursor, determining a location for a virtual cursor to be displayed on a second navigational map GUI display corresponding to the geographic reference point on the first navigational map GUI display and concurrently displaying the virtual cursor at the determined location overlying the second navigational map.

Abstract: A nitrogen-oxide (NOx) sensor control system includes a NOx sensor analog front-end, a temperature sensor analog front-end, and a processing system. The NOx sensor analog front-end is adapted to receive analog NOx sensor signals from a NOx sensor and is configured to convert the analog NOx sensor signals to digital NOx sensor signals. The temperature sensor analog front-end is adapted to receive analog temperature sensor signals from a temperature sensor and is configured to convert the analog temperature sensor signals to digital temperature sensor signals. The processing system is coupled to receive the digital NOx sensor signals and the digital temperature sensor signals and is configured, in response thereto, to: supply the digital NOx sensor signals to an external system, and control a flow of current to a heater element in the NOx sensor.

Abstract: A microelectromechanical systems (MEMS) device and a light assembly that includes the MEMS device. The MEMS device includes a first arm, a second arm, at least one permanent magnet, a fan structure, and a coil. The first arm has a first arm first end and a first arm second end. The second arm is coupled to, and is spaced apart from, the first arm and has a second arm first end and a second arm second end. The at least one permanent magnet is coupled to the first arm second end. The fan structure is coupled to, and extends in cantilever manner from, the second arm second end and includes a connection end and a free end. The coil is disposed on or within the fan structure. When the coil is electrically energized, a Lorentz force is generated that causes the fan structure to vibrate relative to the permanent magnet.

Abstract: In some examples, a system includes a magnet configured to move in response to a movement of a wear pin indicator of a brake assembly of a vehicle; and a sensor configured to generate position data corresponding to the magnet, the position data indicating a relative linear position of the wear pin indicator, wherein the position data corresponds to an estimated remaining useful lifespan of the brake assembly. Additionally, the system includes an energy harvesting device configured to generate an electrical signal based on an operation of one or both of the brake assembly and the vehicle, wherein the energy harvesting device is configured to deliver at least a portion of the electrical signal to the sensor.

Abstract: The present utility model relates to a device for improving gas detection in a photoionization detector. A gas detector is provided. The device reduces interference of photoelectric noise on the reading of the gas detector for target gases such as volatile organic compounds.

Abstract: Methods and systems are provided for assisting operation of a vehicle using speech recognition. One method involves automatically identifying an input element based at least in part on an audio communication with respect to the vehicle, identifying one or more constraints associated with the input element, obtaining a limited command vocabulary for the input element using the one or more constraints, and automatically constructing a contextual speech recognition graph for the input element prior to user selection of the input element using the limited command vocabulary. Thereafter, subsequently received audio input is recognized using the contextual speech recognition graph that was automatically and prospectively generated.

Abstract: Methods and systems for authenticating operations of an aircraft are disclosed. In at least one embodiment, the method may include: receiving, by an aircraft data gateway, a request for an operation of an aircraft from an operations portal; performing a first digital authentication of the request using first digital authentication information; performing a second digital authentication of the request using second digital authentication information, the second digital authentication information being distinct from the first digital authentication information; and executing the operation of the aircraft upon validating the first digital authentication and the second digital authentication.

Abstract: An actuator assembly includes an actuator drive source and a gust lock. The actuator drive source is operable to supply an actuator drive torque to drive a component. The gust lock is movable between a locked position, in which rotation of the drive source is prevented, and an unlocked position, in which rotation of the drive source is not prevented. The gust lock includes a lock shaft, a lock rotor, a lock motor, and a linear actuator. The lock shaft is rotatable with the drive source when the gust lock is in the unlocked position. The lock rotor is rotatable with the lock shaft. The lock motor is configured to supply a lock drive torque. The linear actuator is coupled to receive the lock drive torque and is configured, upon receipt of the lock drive torque, to move between an engaged position and a disengaged position.

Abstract: An optical frequency comb generation system includes an optical waveguide portion having a uniform width, a first chirped Bragg grating disposed at one end of the optical waveguide portion and a second chirped Bragg grating disposed at the other end of the optical waveguide portion. The first chirped Bragg grating includes at least a first periodic variation having a first refractive index and a second periodic variation having a second refractive index. The second chirped Bragg grating includes the at least first and second periodic variations. A first cavity associated with a first resonant frequency extends between the first periodic variation of the first chirped Bragg grating and the first periodic variation of the second chirped Bragg grating. A second cavity associated with a second resonant frequency extends between the second periodic variation of the first chirped Bragg grating and the second periodic variation of the second chirped Bragg grating.

Abstract: Methods and systems are provided for resolving a user input. One method involves assigning a first identifier to a first stream of messages from a user input device corresponding to a first user input with respect to an application, and while a user interaction state associated with the first stream of messages is active, assigning a second identifier to a second stream of messages from the user input device, and in response to detecting the second identifier corresponds to the first identifier, deactivating the first stream of messages associated with the first stream of messages, wherein deactivating the first stream of messages results in the application responding to the second stream of messages corresponding to the second user input.

Abstract: A multilayer mirror comprises a reflector section including a plurality of alternating layers of a high index material and a low index material, and a filter section over the reflector section. The filter section comprises a first filter layer including a low index material on a layer of high index material of the reflector section; a second filter layer on the first filter layer, the second filter layer comprising a high index material that is different than the high index material in the reflector section; and a third filter layer on the second filter layer, the third filter layer comprising a low index material. Each filter layer has an optical thickness greater than or equal to the optical thickness of each layer of the alternating layers. The filter section substantially blocks ultraviolet (UV) energy, thereby preventing UV energy from substantially impinging on the high index material of the reflector section.

Abstract: An integrated energy optimizer having an edge side and a cloud side. The edge side may incorporate an energy optimizer, a building management system connected to the energy optimizer, a controller connected to the building management system, and equipment connected to the controller. The cloud side may have a cloud connected to the energy optimizer and to the building management system, and a user interface connected to the cloud. Data from the field sensor may go to the optimizer and the building management system. The data may be processed at the optimizer and the building management system for proper settings at the building management system.

Abstract: A system and method for determining a lateral and vertical path for aircraft guidance from a current aircraft position to a landing runway following a complete loss of engine thrust includes determining, in a processing system, a final approach segment, a deceleration segment, and a driftdown segment. Connecting, in the processing system, the driftdown segment to the deceleration segment, and the deceleration segment to the final approach segment, to form a complete lateral and vertical path from the current aircraft position to the landing runway. And rendering, on a display device, a graphical representation of the complete lateral and vertical path from the current aircraft position to the landing runway, wherein the graphical representation of the complete lateral and vertical path updates as the aircraft travels.