A system and method for vehicle compartment item presence indication senses an item within a vehicle compartment and notifies a user if the item is expected or unexpected within the compartment based on a vehicle state. Should the item be expected in a compartment during a phase of flight where the compartment is expected to contain items, there is no abnormal indication. However, if a compartment is expected to be empty during a specific phase of flight and the sensors indicate an item is present, the system will alert the user to the unexpected item.

Systems and methods for coordinating with a flight management system (FMS) on-board an aircraft to determine whether a flight plan (FP) change generated by an external device is valid. The method includes generating the FP change, which includes a deviation to the intended FP and a savings parameter associated with a parameter of the intended FP, responsive to weather data and aircraft state data; generating a lateral display showing the intended FP and an alphanumeric window with the FP change; transmitting the FP change to the FMS; receiving, from the FMS, a travel path and a calculated parameter for the travel path, generated by the FMS responsive to the FP change; determining whether the travel path realizes the savings parameter by comparing the calculated parameter to the savings parameter; and, displaying either a selectable graphical user interface (GUI) object to implement the FP change, or a warning based thereon.

Systems and methods for coordinating with a flight management system (FMS) on-board an aircraft to determine whether a flight plan (FP) change generated by an external device is valid. The method includes generating the FP change, which includes a deviation to the intended FP and a savings parameter associated with a parameter of the intended FP, responsive to weather data and aircraft state data; generating a lateral display showing the intended FP and an alphanumeric window with the FP change; transmitting the FP change to the FMS; receiving, from the FMS, a travel path and a calculated parameter for the travel path, generated by the FMS responsive to the FP change; determining whether the travel path realizes the savings parameter by comparing the calculated parameter to the savings parameter; and, displaying either a selectable graphical user interface (GUI) object to implement the FP change, or a warning based thereon.

Systems and methods enabling user control over use of aircraft sensors located onboard an aircraft. The method receives sensor signals comprising any combination of ADS signals, IRS signals and a third RA signals, and GPS signals; comparing sensor data values in the sensor signals to each other and to respective acceptable thresholds and critical thresholds that are preprogrammed; grouping avionic systems on-board the aircraft into subgroups having a same sensor reliance; presenting a graphical user interface (GUI) page on the display system, the GUI page identifying a sensor subgroup, the aircraft sensors of the respective sensor subgroup, and respective critical sensor parameters and associated critical sensor parameter data; visually distinguishing an critical sensor parameter data that exceeds the respective acceptable threshold or exceeds the respective critical threshold; and, accepting user deselections of aircraft sensors via the GUI page.

Systems and methods enabling user control over use of aircraft sensors located onboard an aircraft. The method receives sensor signals comprising any combination of ADS signals, IRS signals and a third RA signals, and GPS signals; comparing sensor data values in the sensor signals to each other and to respective acceptable thresholds and critical thresholds that are preprogrammed; grouping avionic systems on-board the aircraft into subgroups having a same sensor reliance; presenting a graphical user interface (GUI) page on the display system, the GUI page identifying a sensor subgroup, the aircraft sensors of the respective sensor subgroup, and respective critical sensor parameters and associated critical sensor parameter data; visually distinguishing an critical sensor parameter data that exceeds the respective acceptable threshold or exceeds the respective critical threshold; and, accepting user deselections of aircraft sensors via the GUI page.

An indicator for monitoring temperature and wear of one or more aircraft brakes. One or more sensors are provided for sensing a parameter of usage, and an estimate of usage of the part can be determined based upon the signal indicating the sensed value of the parameter of usage of the aircraft part. A plurality of sensors can be provided for sensing usage of a plurality of parts of the aircraft, and the estimate of usage of the part can be stored for access of the estimate by ground personnel. In addition, the sensed usage data are critical inputs for the brake controller to regulate which brakes are applied.

An aircrew automation system that provides a pilot with high-fidelity knowledge of the aircraft's physical state, and notifies that pilot of any deviations in expected state based on predictive models. The aircrew automation may be provided as a non-invasive ride-along aircrew automation system that perceives the state of the aircraft through visual techniques, derives the aircraft state vector and other aircraft information, and communicates any deviations from expected aircraft state to the pilot.

An aircrew automation system that provides a pilot with high-fidelity knowledge of the aircraft's physical state, and notifies that pilot of any deviations in expected state based on predictive models. The aircrew automation may be provided as a non-invasive ride-along aircrew automation system that perceives the state of the aircraft through visual techniques, derives the aircraft state vector and other aircraft information, and communicates any deviations from expected aircraft state to the pilot.

The present disclosure provides methods for forming sol-gels, sol-gel films and substrates, such as vehicle components, having a sol-gel film disposed thereon. At least one method of forming a sol-gel includes mixing a metal alkoxide, an acid stabilizer, and an organic solvent to form a first mixture having about 10 wt % or less water content based on the total weight of the first mixture. The method includes mixing an organosilane with the first mixture to form a second mixture having about 10 wt % or less water content based on the total weight of the second mixture.

Aspects of the disclosure relate to identifying and responding to problem conditions for a fleet of aerial vehicles. This may include receiving at one or more processors of one or more server computing devices sensor feedback from an AV of the fleet. A problem condition may be identified using the sensor feedback. A mitigation response for the problem condition relating to a mission assigned to the aerial vehicle may be determined. The mitigation response may be sent to the AV in order to cause the aerial vehicle to maneuver according to the mitigation response and thereby automatically respond to the problem condition.