aerosandbox.library.gust_pitch_control
======================================

.. py:module:: aerosandbox.library.gust_pitch_control


Attributes
----------

.. autoapisummary::

   aerosandbox.library.gust_pitch_control.N


Classes
-------

.. autoapisummary::

   aerosandbox.library.gust_pitch_control.TransverseGustPitchControl


Module Contents
---------------

.. py:class:: TransverseGustPitchControl(reduced_time, gust_profile, velocity)

   Bases: :py:obj:`aerosandbox.common.ImplicitAnalysis`


   An implicit analysis that calculates the optimal pitching maneuver
   through a specified transverse gust, with the goal of minimzing the
   deviation from a specified lift coefficient. It utilizes differentiable
   duhamel superposition integrals for Kussner's gust model and Wagner's
   pitching model, as well as any additional lift from the added mass.

   :param reduced_time: Reduced time, equal to the number of semichords travelled. See function reduced_time in the unsteady aero library
   :type reduced_time: np.ndarray
   :param gust_profile: An array that specifies the gust velocity at each reduced time
   :type gust_profile: np.ndarray
   :param velocity: The velocity of the aircraft
   :type velocity: float


   .. py:attribute:: reduced_time


   .. py:attribute:: gust_profile


   .. py:attribute:: timesteps


   .. py:attribute:: velocity


   .. py:method:: _setup_unknowns()


   .. py:method:: _enforce_governing_equations()


   .. py:method:: calculate_transients()


.. py:data:: N
   :value: 100