Struct LcrnsSatConfig

Struct Documentation

struct LcrnsSatConfig

Initial Cartesian state of one LCRNS / LunaNet relay satellite, defined at the scenario start epoch in the Moon-centered inertial frame (Frame::MOON_CI), e.g. taken from the NASA LCRNS reference constellation. Shared by the surface-rover and lander navigation applications (relays are propagated as Keplerian orbits app-internally).

Public Members

std::string name = "SV"
Vec3d r0_m = Vec3d::Zero()

initial position [m], Frame::MOON_CI.

Vec3d v0_mps = Vec3d::Zero()

initial velocity [m/s], Frame::MOON_CI.