Struct inertialsim::examples::nesc::FlightData¶
ClassList > inertialsim > examples > nesc > FlightData
NESC flight simulation data. More...
#include <nesc.h>
Public Attributes¶
| Type | Name |
|---|---|
| Vector3D | angular_rate Angular rate of body frame relative to inertial frame in rad/s. |
| EulerAngles | attitude Attitude as Euler angles (roll, pitch, yaw) in radians. |
| Scalar1D | gravitation Local gravitation (excluding centripetal forces) in m/s/s. |
| Vector3D | position |
| Timestamps | time Timestamps (s) from simulation. |
| Vector3D | velocity Velocity in NED frame (North, East, Down) in m/s. |
Detailed Description¶
Flight simulation data from an NESC atmospheric check case. This is a subset of the original data. Not all check cases contain the same variables and only variables relevant to InertialSim are loaded from the source data.
Data from the NASA Engineering and Safety Center (NESC) simulations. See Reference [19] for more information.
Public Attributes Documentation¶
variable angular_rate¶
Angular rate of body frame relative to inertial frame in rad/s.
variable attitude¶
Attitude as Euler angles (roll, pitch, yaw) in radians.
variable gravitation¶
Local gravitation (excluding centripetal forces) in m/s/s.
variable position¶
Position in geodetic coordinates (lat, lon, alt) where lat/lon are in radians and altitude MSL is in meters.
variable time¶
Timestamps (s) from simulation.
variable velocity¶
Velocity in NED frame (North, East, Down) in m/s.
The documentation for this class was generated from the following file cpp/include/inertialsim/examples/nesc.h