Patent classifications
G01C5/06
TIMEPIECE MECHANISM INDICATING INFORMATION RELATING TO AN AMBIENT PRESSURE COMPRISING A ZERO-RESET MECHANISM AND TIMEPIECE, SUCH AS A DIVING WATCH, COMPRISING SUCH A MECHANISM
Provided is a timepiece mechanism (1, 1′) indicating information relating to the ambient pressure. The timepiece includes an ambient pressure measuring device that deforms mechanically due to ambient pressure variation. The device includes a first wheel assembly (31) kinematically linked to the ambient pressure measuring device that rotates under the effect of an ambient pressure variation and a measured pressure indicator mechanism (40) including a measured pressure indicator organ. The device also includes a second wheel assembly (33) configured to be in uncouplable connection with the first wheel assembly (31) so thesecond wheel assembly (33) is rotated by the first wheel assembly (31) under the effect of the pressure variation. Also included is a zero-reset mechanism (100) to position the measured pressure indicator organ (44) in a reference position by uncoupling the second wheel assembly (33) from the first wheel assembly (31).
TIMEPIECE MECHANISM INDICATING INFORMATION RELATING TO AN AMBIENT PRESSURE COMPRISING A ZERO-RESET MECHANISM AND TIMEPIECE, SUCH AS A DIVING WATCH, COMPRISING SUCH A MECHANISM
Provided is a timepiece mechanism (1, 1′) indicating information relating to the ambient pressure. The timepiece includes an ambient pressure measuring device that deforms mechanically due to ambient pressure variation. The device includes a first wheel assembly (31) kinematically linked to the ambient pressure measuring device that rotates under the effect of an ambient pressure variation and a measured pressure indicator mechanism (40) including a measured pressure indicator organ. The device also includes a second wheel assembly (33) configured to be in uncouplable connection with the first wheel assembly (31) so thesecond wheel assembly (33) is rotated by the first wheel assembly (31) under the effect of the pressure variation. Also included is a zero-reset mechanism (100) to position the measured pressure indicator organ (44) in a reference position by uncoupling the second wheel assembly (33) from the first wheel assembly (31).
Constraining barometric pressure sensor calibration with sporadic data collection
Multiple calibration results for calibrating a barometric pressure sensor based on data received from a device containing the sensor are determined and stored in a table. The table is updated based on rules regarding a relationship between each calibration result and a current calibration value. The calibration results are weighted and combined to determine a combined calibration result. The calibration value for calibrating the sensor is selected from the calibration results, the combined calibration results, or the current calibration value based on a selection criteria.
Constraining barometric pressure sensor calibration with sporadic data collection
Multiple calibration results for calibrating a barometric pressure sensor based on data received from a device containing the sensor are determined and stored in a table. The table is updated based on rules regarding a relationship between each calibration result and a current calibration value. The calibration results are weighted and combined to determine a combined calibration result. The calibration value for calibrating the sensor is selected from the calibration results, the combined calibration results, or the current calibration value based on a selection criteria.
SYSTEM AND METHOD FOR INDOORS ALTITUDE DETERMINATION
Altitude determining circuitry for use in a User Equipment (UE) of a wireless communication network is provided. The circuitry comprises a receiver to receive at least one pressure parameter representative of a plurality of indoors pressure measurements from a respective plurality of indoors pressure measurement units located inside a building at different altitudes. The altitude determining circuitry also has processing circuitry to receive from a pressure sensor in the User Equipment a local pressure measurement at the UE and the processor determines an indoors altitude of the UE using the at least one pressure parameter and the UE local pressure. An integrated circuit for a Global Navigate Satellite System comprising the altitude determining circuitry and an indoors pressure measurement unit having a sensor for making a pressure measurement and a transmitter for transmitting the pressure measurement to the UE or to a further indoors pressure measurement unit are also provided.
SYSTEM AND METHOD FOR INDOORS ALTITUDE DETERMINATION
Altitude determining circuitry for use in a User Equipment (UE) of a wireless communication network is provided. The circuitry comprises a receiver to receive at least one pressure parameter representative of a plurality of indoors pressure measurements from a respective plurality of indoors pressure measurement units located inside a building at different altitudes. The altitude determining circuitry also has processing circuitry to receive from a pressure sensor in the User Equipment a local pressure measurement at the UE and the processor determines an indoors altitude of the UE using the at least one pressure parameter and the UE local pressure. An integrated circuit for a Global Navigate Satellite System comprising the altitude determining circuitry and an indoors pressure measurement unit having a sensor for making a pressure measurement and a transmitter for transmitting the pressure measurement to the UE or to a further indoors pressure measurement unit are also provided.
SYSTEMS AND METHODS FOR ESTIMATING A DIFFERENCE IN HEIGHT BETWEEN TWO FLOORS IN A BUILDING FOR USE IN ESTIMATING A HEIGHT OR AN ALTITUDE OF ONE OF THE TWO FLOORS
Estimating a difference in height between floors in a building for use in estimating a height or an altitude of one of the floors. A height difference is estimated between a first floor and a second floor based on outdoor temperatures of first and second time periods, an indoor temperature of the first or second time period, and first and second estimated differences in height between the first and second floors that is based on measurements of pressure from mobile devices when the mobile devices were on the first and second floors during the first and second time periods.
SYSTEMS AND METHODS FOR ESTIMATING A DIFFERENCE IN HEIGHT BETWEEN TWO FLOORS IN A BUILDING FOR USE IN ESTIMATING A HEIGHT OR AN ALTITUDE OF ONE OF THE TWO FLOORS
Estimating a difference in height between floors in a building for use in estimating a height or an altitude of one of the floors. A height difference is estimated between a first floor and a second floor based on outdoor temperatures of first and second time periods, an indoor temperature of the first or second time period, and first and second estimated differences in height between the first and second floors that is based on measurements of pressure from mobile devices when the mobile devices were on the first and second floors during the first and second time periods.
UNMANNED AIRCRAFT
The present disclosure relates to an unmanned aircraft capable of suitably limiting a variation in pressure altitude.
The unmanned aircraft includes a housing that constitutes a main body, one barometric pressure sensor that is provided in one space formed inside the housing, and four or more openings that have substantially the same opening area, the four or more openings being arranged in a balanced manner over an entire circumference of a side portion of the housing. The present disclosure can be applied to a drone including a barometric pressure sensor.
UNMANNED AIRCRAFT
The present disclosure relates to an unmanned aircraft capable of suitably limiting a variation in pressure altitude.
The unmanned aircraft includes a housing that constitutes a main body, one barometric pressure sensor that is provided in one space formed inside the housing, and four or more openings that have substantially the same opening area, the four or more openings being arranged in a balanced manner over an entire circumference of a side portion of the housing. The present disclosure can be applied to a drone including a barometric pressure sensor.