Util module¶
Function helpers.
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poliastro.util.circular_velocity(k, a)¶ Compute circular velocity for a given body (k) and semimajor axis (a).
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poliastro.util.norm(vec)¶ Norm of a Quantity vector that respects units.
Parameters: vec (Quantity) – Vector with units.
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poliastro.util.time_range(start, *, periods=50, spacing=None, end=None, format=None, scale=None)¶ Generates range of astronomical times.
New in version 0.8.0.
Parameters: - periods (int, optional) – Number of periods, default to 50.
- spacing (Time or Quantity, optional) – Spacing between periods, optional.
- end (Time or equivalent, optional) – End date.
Returns: Array of time values.
Return type: Time
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poliastro.util.hyp_nu_limit(ecc, r_max_ratio=inf)¶ Limit true anomaly for hyperbolic orbits.
Parameters:
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poliastro.util.get_eccentricity_critical_argp(attractor, a, inc)¶ Calculates the eccentricity for frozen orbits when the argument of perigee is critical
Parameters:
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poliastro.util.get_inclination_critical_argp(attractor, a, ecc)¶ Calculates the inclination for frozen orbits when the argument of perigee is critical and the eccentricity is given
Parameters:
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poliastro.util.get_eccentricity_critical_inc(ecc=None)¶ Calculates the eccentricity when a frozen orbit has critical inclination
If ecc is None we set an arbitrary value which is the Moon ecc because it seems reasonable
Parameters: ecc (: ~astropy.units.Quantity, optional) – Eccentricity, or None if it was not defined
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poliastro.util.find_closest_value(value, values)¶ Calculates the closest value in the given values :param value: :type value: ~astropy.units.Quantity :param values: :type values: ~astropy.units.Quantity