record

Avionics.NavigationEstimate

Estimator-independent state consumed by guidance and control

Public declarations

Explicit source declarations; dimensions, modifications and defaults are shown as written, without evaluation.

Role	Name	Type	Dimensions / attributes / default	Description
field	`valid`	`Boolean`
field	`timestamp_s`	`Real`	`(unit = "s")`
field	`positionWorldEnu_m`	`Real`	`[3](each unit = "m")`
field	`velocityWorldEnu_m_s`	`Real`	`[3](each unit = "m/s")`
field	`accelerationWorldEnu_m_s2`	`Real`	`[3](each unit = "m/s2")`
field	`quaternionWorldBody`	`Real`	`[4](each unit = "1")`	Scalar-first Hamilton quaternion {w,x,y,z}, body FLU to world ENU
field	`rotationWorldBody`	`Real`	`[3, 3](each unit = "1")`	Direction-cosine matrix mapping body FLU vectors into world ENU
field	`eulerRpy_rad`	`Real`	`[3](each unit = "rad")`	Intrinsic 3-2-1 attitude ordered {roll,pitch,yaw}
field	`angularVelocityBodyFlu_rad_s`	`Real`	`[3](each unit = "rad/s")`
field	`angularVelocityWorldEnu_rad_s`	`Real`	`[3](each unit = "rad/s")`

Modelica declarations and implementation

Show parameters, interfaces and source

Parameters, inputs, outputs, defaults and equations from the source file.

record NavigationEstimate
    "Estimator-independent state consumed by guidance and control"
    Boolean valid;
    Real timestamp_s(unit = "s");
    Real positionWorldEnu_m[3](each unit = "m");
    Real velocityWorldEnu_m_s[3](each unit = "m/s");
    Real accelerationWorldEnu_m_s2[3](each unit = "m/s2");
    Real quaternionWorldBody[4](each unit = "1")
      "Scalar-first Hamilton quaternion {w,x,y,z}, body FLU to world ENU";
    Real rotationWorldBody[3, 3](each unit = "1")
      "Direction-cosine matrix mapping body FLU vectors into world ENU";
    Real eulerRpy_rad[3](each unit = "rad")
      "Intrinsic 3-2-1 attitude ordered {roll,pitch,yaw}";
    Real angularVelocityBodyFlu_rad_s[3](each unit = "rad/s");
    Real angularVelocityWorldEnu_rad_s[3](each unit = "rad/s");
  end NavigationEstimate;