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stability

hpr_sim::metrics

Function stability 

Source 
pub fn stability(
    aero: &AeroModel,
    time_s: f64,
    height_above_ground_m: f64,
    dynamic_pressure_pa: f64,
    cg_station_m: f64,
    mach: f64,
) -> Result<Stability, SimError>
Expand description

The static margin and the flight margin of aero at time_s, with the center of mass height_above_ground_m above the launch site and at cg_station_m on the airframe, and the flight’s air at Mach mach pressing with dynamic_pressure_pa.

§Errors

As margin.