Source code for rocketpy.exceptions

"""Custom exceptions and warnings for RocketPy."""




class RocketPyError(Exception):
    """Base class for all RocketPy exceptions."""





class InvalidParameterError(RocketPyError, ValueError):
    """Raised when a constructor parameter has an invalid value (e.g. negative
    radius or mass)."""





class InvalidInertiaError(RocketPyError, ValueError):
    """Raised when the inertia tuple/list does not have the expected length."""





class UnstableRocketWarning(UserWarning):
    """Issued when the rocket's static margin is negative at motor ignition,
    indicating an aerodynamically unstable configuration.

    Not issued when the rocket has any ``GenericSurface`` aerodynamic
    surfaces, since their lift coefficient derivative is not accounted for
    in the center of pressure calculation, making the static margin
    unreliable for this check in that case.
    """