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Update navsat proto to include covariance #489

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57 changes: 49 additions & 8 deletions proto/gz/msgs/navsat.proto
Original file line number Diff line number Diff line change
Expand Up @@ -26,30 +26,71 @@ option java_outer_classname = "NavSatProtos";
/// This replaces the GPS message.

import "gz/msgs/header.proto";
import "gz/msgs/double_v.proto";

message NavSat
{
/// \brief Optional header data
Header header = 1;
Header header = 1;

/// \brief Latitude in degrees
double latitude_deg = 2;
double latitude_deg = 2;

/// \brief Longitude in degrees
double longitude_deg = 3;
double longitude_deg = 3;

/// \brief Altitude in meters
double altitude = 4;
double altitude = 4;

/// \brief Covariance or dilution of precision (DoP) 9 of the position
/// Position covariance [m^2] defined relative to a tangential plane
/// through the reported position. The components are East, North, and
/// Up (ENU), in row-major order.
/// For more information see From Global Positioning System: Signals,
/// Measurements, and Performance section 6.1.2
Double_V position_covariance = 5;

/// \brief Position covariance information availability
/// If the Dilution of Precision or covariance of the fix is known, fill
/// it in completely. If the GPS receiver provides the variance of each
/// measurement, put them along the diagonal. If only DoP parameters are
/// available, estimate an approximate covariance from that.
/// Possible values are:
/// - COVARIANCE_TYPE_UNKNOWN = 0
/// - COVARIANCE_TYPE_APPROXIMATED = 1
/// - COVARIANCE_TYPE_DIAGONAL_KNOWN = 2
/// - COVARIANCE_TYPE_KNOWN = 3
uint32 position_covariance_type = 6;

/// \brief East velocity in the ENU frame, in m / s
double velocity_east = 5;
double velocity_east = 7;

/// \brief North velocity in the ENU frame, in m / s
double velocity_north = 6;
double velocity_north = 8;

/// \brief Up velocity in the ENU frame, in m / s
double velocity_up = 7;
double velocity_up = 9;

/// \brief Covariance or dilution of precision (DoP) 9 of the velocity
/// Position covariance [(m/s)^2] defined relative to a tangential plane
/// through the reported position. The components are East, North, and
/// Up (ENU), in row-major order.
/// For more information see From Global Positioning System: Signals,
/// Measurements, and Performance section 6.2.1
Double_V velocity_covariance = 10;

/// \brief Velocity covariance information availability
/// If the Dilution of Precision or covariance of the fix is known, fill
/// it in completely. If the GPS receiver provides the variance of each
/// measurement, put them along the diagonal. If only DoP parameters are
/// available, estimate an approximate covariance from that.
/// Possible values are:
/// - COVARIANCE_TYPE_UNKNOWN = 0
/// - COVARIANCE_TYPE_APPROXIMATED = 1
/// - COVARIANCE_TYPE_DIAGONAL_KNOWN = 2
/// - COVARIANCE_TYPE_KNOWN = 3
uint32 velocity_covariance_type = 11;

/// \brief ID of reference frame
string frame_id = 8;
string frame_id = 12;
}