A method can include receiving sensor data, receiving satellite observations, determining a positioning solution (e.g., PVT solution, PVA solution, kinematic parameters, etc.) based on the sensor data and the satellite observations. A system can include a sensor, a GNSS receiver, and a processor configured to determine a positioning solution based on readings from the sensor and the GNSS receiver.

A method can include receiving sensor data, receiving satellite observations, determining a positioning solution (e.g., PVT solution, PVA solution, kinematic parameters, etc.) based on the sensor data and the satellite observations. A system can include a sensor, a GNSS receiver, and a processor configured to determine a positioning solution based on readings from the sensor and the GNSS receiver.

The invention relates to a method for estimating the attitude (A) of a vehicle (1000) by using a global navigation satellite system, GNSS, (2000) having a plurality of satellites (2010, 2020, 2030, 2040), wherein the vehicle comprises at least a first antenna (1200) and a second antenna (1210) having a separation (d) to each other, comprising the steps of: detecting that said vehicle is moving and not turning and obtaining a heading using the GNSS; calculating an integer ambiguity fix corresponding to the relative position vector of the antennas using said heading the separation (d); determining the attitude of the vehicle, including validating candidate values of the attitude obtained from the GNSS by analysing residuals in respect of the relative position vector.

A hydraulic excavator includes a receiver configured to calculate a position and an azimuth angle of an upper swing structure on the basis of satellite signals received by two GNSS antennae and a controller configured to calculate a distal end position of a bucket on the basis of the position and the azimuth angle of the upper swing structure calculated by the receiver. The controller sets, on the basis of installation positions of the two GNSS antennae, a movable range of a front work device and an inclination angle and an azimuth angle of the upper swing structure, a range within which the front work device possibly becomes an obstacle to reception of satellite signals by each of the two GNSS antennae as a mask range. The receiver is configured to calculate the position and the azimuth angle of the upper swing structure on the basis of the satellite signals transmitted from the remaining satellites other than the satellites positioned in the mask range.

A hydraulic excavator includes a receiver configured to calculate a position and an azimuth angle of an upper swing structure on the basis of satellite signals received by two GNSS antennae and a controller configured to calculate a distal end position of a bucket on the basis of the position and the azimuth angle of the upper swing structure calculated by the receiver. The controller sets, on the basis of installation positions of the two GNSS antennae, a movable range of a front work device and an inclination angle and an azimuth angle of the upper swing structure, a range within which the front work device possibly becomes an obstacle to reception of satellite signals by each of the two GNSS antennae as a mask range. The receiver is configured to calculate the position and the azimuth angle of the upper swing structure on the basis of the satellite signals transmitted from the remaining satellites other than the satellites positioned in the mask range.

Three or more receivers installed in a UAV receive signals from a number of satellites, and generate, based on these received signals, observation data items including information items about distances from the satellites to the receivers. An information processing apparatus calculates, based on these observation data items and on position data items of the plurality of satellites, estimated reception positions at which one or more of the receivers are estimated to receive the signals from the satellites. The information processing apparatus calculates, based on these estimated reception positions and on an estimated posture of the UAV, estimated positions of a ranging apparatus in the UAV. The ranging apparatus measures a distance to a target by applying a laser beam to the target in synchronization with timings at which the receivers receives the signals from the satellites.

A method for estimating the attitude of a vehicle by using a global navigation satellite system having a plurality of satellites, wherein the vehicle comprises at least a first antenna and a second antenna having a separation to each other, comprising the steps of: detecting an outage of said global navigation satellite system; starting a dead-reckoning algorithm in order to extrapolate a change in attitude during the outage of said global navigation satellite system obtaining a dead-reckoned attitude; detecting that said global navigation satellite system has recovered, in particular via the availability of carrier phase observables and calculating a new attitude using the recovered global navigation satellite system by incorporating the obtained dead-reckoned attitude as a starting condition.

A method for estimating the attitude of a vehicle by using a global navigation satellite system having a plurality of satellites, wherein the vehicle comprises at least a first antenna and a second antenna having a separation to each other, comprising the steps of: detecting an outage of said global navigation satellite system; starting a dead-reckoning algorithm in order to extrapolate a change in attitude during the outage of said global navigation satellite system obtaining a dead-reckoned attitude; detecting that said global navigation satellite system has recovered, in particular via the availability of carrier phase observables and calculating a new attitude using the recovered global navigation satellite system by incorporating the obtained dead-reckoned attitude as a starting condition.

An information collection apparatus collects information items about a position and a posture while flying in the air under a state of being attached to a drone. The information collection apparatus includes: six receivers, each of which receives location signals that are broadcasted from a plurality of satellites; and a frame to which six antennas of the six receivers are fixed. The six antennas of the six receivers, which receive the location signals, are arranged in an annular array and at equal intervals. The six receivers each receive the location signals that are broadcasted from the satellites. Thus, even without use of an IMU, by using these signals received by the receivers, the position and the posture can be estimated with high accuracy.

A system and method for determining an orientation of a firearm includes a first position sensor, a second position sensor and a transmitter. The first position sensor can be disposed at a first location on the firearm. The second position sensor can be disposed at a second location on the firearm. The first and second locations can be distinct and define a line parallel to an axis of a barrel of the firearm. The transmitter can be configured to communicate a signal. The first and second position sensors receive the signal from the transmitter and determine one of an orientation and a heading of the firearm based on the signal.