A barrier data collection device includes a unit estimation unit that estimates, based on sensor data with position information including height at a time when a mobile body including a flying mobile body moving in the air moves, the sensor data being collected in advance about each of geographical ranges, with an estimator, about each of sets of the geographical ranges and heights included in the sensor data in a predetermined time unit, a barrier state obtained by estimating a state of which of barrier types the set is, a shape estimation unit that estimates, about a set satisfying a condition among the sets, a barrier shape based on the sensor data and an estimation result of the barrier state estimated about each of the sets in the time unit, and a barrier estimation unit that estimates, based on the estimation result of the barrier state estimated about the each of the sets, the estimated barrier shape, and a correct answer ratio of the estimator calculated in advance, a probability for each of the barrier types corresponding to each of the sets and estimates the barrier type corresponding to the set from the estimated probability for each of the barrier types.

Provided is a parachute device capable of reliably opening a parachute. A parachute device includes a parachute, a parachute accommodation section formed in a tubular shape including an opening at one end and a bottom at another end, the parachute accommodation section being configured to accommodate the parachute inside the parachute accommodation section, at least one flying body formed in a tubular shape including an opening at one end and a bottom at another end, the flying body being connected to the parachute, a tubular ejection section fixed at the parachute accommodation section, and configured to hold the flying body and eject the held flying body, a gas generating device fixed at the parachute accommodation section, and configured to generate gas, and a gas introduction path configured to introduce the gas generated from the gas generating device to an interior of the ejection section, wherein at the ejection section, one open end portion of the ejection section is inserted into the flying body, and another open end portion of the ejection section communicates with the gas introduction path.

Provided is a parachute device capable of reliably opening a parachute. A parachute device includes a parachute, a parachute accommodation section formed in a tubular shape including an opening at one end and a bottom at another end, the parachute accommodation section being configured to accommodate the parachute inside the parachute accommodation section, at least one flying body formed in a tubular shape including an opening at one end and a bottom at another end, the flying body being connected to the parachute, a tubular ejection section fixed at the parachute accommodation section, and configured to hold the flying body and eject the held flying body, a gas generating device fixed at the parachute accommodation section, and configured to generate gas, and a gas introduction path configured to introduce the gas generated from the gas generating device to an interior of the ejection section, wherein at the ejection section, one open end portion of the ejection section is inserted into the flying body, and another open end portion of the ejection section communicates with the gas introduction path.

An automatic parking lot management system includes an infrastructure sensor for detecting a preset range in a parking lot. A mobile body including a peripheral detection sensor is used, and the mobile body is able to be moved to a detectable position at which the peripheral detection sensor of the mobile body is able to detect a detection range of the infrastructure sensor. When determination is made that there is an abnormality in the infrastructure sensor, the mobile body is moved to the detectable position to cause the peripheral detection sensor to detect the detection range of the infrastructure sensor.

An automatic parking lot management system includes an infrastructure sensor for detecting a preset range in a parking lot. A mobile body including a peripheral detection sensor is used, and the mobile body is able to be moved to a detectable position at which the peripheral detection sensor of the mobile body is able to detect a detection range of the infrastructure sensor. When determination is made that there is an abnormality in the infrastructure sensor, the mobile body is moved to the detectable position to cause the peripheral detection sensor to detect the detection range of the infrastructure sensor.

A method for performing property surveillance via an unmanned aerial vehicle is provided. Surveillance of one or more properties via an unmanned aerial vehicle is obtained. A geofence that determines boundaries of one of the properties is created using the surveillance. Surveillance outside the geofence for the property is blurred. The blurred surveillance is provided to an owner of that property.

A method for performing property surveillance via an unmanned aerial vehicle is provided. Surveillance of one or more properties via an unmanned aerial vehicle is obtained. A geofence that determines boundaries of one of the properties is created using the surveillance. Surveillance outside the geofence for the property is blurred. The blurred surveillance is provided to an owner of that property.

A method of determining one or more fuel characteristics of an aviation fuel for powering a gas turbine engine of an aircraft includes: measuring one or more trace substance parameters of the fuel, the one or more trace substance parameters each associated with a respective trace substance in the fuel; and determining one or more fuel characteristics of the fuel based on the one or more trace substance parameters. Further, a fuel characteristic determination system, a method of operating an aircraft, and an aircraft.

A method of determining one or more fuel characteristics of an aviation fuel for powering a gas turbine engine of an aircraft includes: measuring one or more trace substance parameters of the fuel, the one or more trace substance parameters each associated with a respective trace substance in the fuel; and determining one or more fuel characteristics of the fuel based on the one or more trace substance parameters. Further, a fuel characteristic determination system, a method of operating an aircraft, and an aircraft.

A switch panel for an aircraft includes a cover and aback plate. A distance from the cover to the back plate is a thickness of the switch panel. In some cases, the thickness is less than about 9.525 mm. A button assembly for a switch panel for an aircraft includes a button base, a button retainer, and a lens. The button base includes a bottom end, a base side, and a transition portion between the bottom end and the base side. In certain cases, the transition portion of the button base is beveled or radiused with a sloped or concave shape.