Merge branch 'master' of https://github.com/OpenMDAO/dymos into times…

…eries_change

docs/dymos_book/_toc.yml

@@ -41,6 +41,7 @@ parts:
     - file: examples/water_rocket/water_rocket
     - file: examples/cart_pole/cart_pole
     - file: examples/brachistochrone/brachistochrone_tandem_phases
+    - file: examples/cannonball_implicit_duration/cannonball_implicit_duration
 - caption: Feature Reference
   chapters:
   - file: features/phases/phases_list

dymos/examples/cannonball/doc/test_doc_cannonball_implicit_duration.py

@@ -0,0 +1,294 @@
+import unittest
+
+import matplotlib.pyplot as plt
+import numpy as np
+
+from openmdao.utils.testing_utils import use_tempdirs, require_pyoptsparse
+
+
+plt.switch_backend('Agg')
+
+
+def initial_guess(t_dur, gam0=np.pi/3):
+    t = np.linspace(0, t_dur, num=100)
+    g = -9.80665
+    v0 = -0.5*g*t_dur/np.sin(gam0)
+    r = v0*np.cos(gam0)*t
+    h = v0*np.sin(gam0)*t + 0.5*g*t**2
+    v = np.sqrt(v0*np.cos(gam0)**2 + (v0*np.sin(gam0) + g*t)**2)
+    gam = np.arctan2(v0*np.sin(gam0) + g*t, v0*np.cos(gam0)**2)
+
+    guess = {'t': t, 'r': r, 'h': h, 'v': v, 'gam': gam}
+
+    return guess
+
+
+@use_tempdirs
+class TestTwoPhaseCannonballForDocs(unittest.TestCase):
+
+    @require_pyoptsparse(optimizer='IPOPT')
+    def test_two_phase_cannonball_for_docs(self):
+        from scipy.interpolate import interp1d
+
+        import openmdao.api as om
+        from openmdao.utils.assert_utils import assert_near_equal
+
+        import dymos as dm
+        from dymos.models.atmosphere.atmos_1976 import USatm1976Data
+
+        #############################################
+        # Component for the design part of the model
+        #############################################
+        class CannonballSizeComp(om.ExplicitComponent):
+            """
+            Compute the area and mass of a cannonball with a given radius and density.
+
+            Notes
+            -----
+            This component is not vectorized with 'num_nodes' as is the usual way
+            with Dymos, but is instead intended to compute a scalar mass and reference
+            area from scalar radius and density inputs. This component does not reside
+            in the ODE but instead its outputs are connected to the trajectory via
+            input design parameters.
+            """
+            def setup(self):
+                self.add_input(name='radius', val=1.0, desc='cannonball radius', units='m')
+                self.add_input(name='dens', val=7870., desc='cannonball density', units='kg/m**3')
+
+                self.add_output(name='mass', shape=(1,), desc='cannonball mass', units='kg')
+                self.add_output(name='S', shape=(1,), desc='aerodynamic reference area', units='m**2')
+
+                self.declare_partials(of='mass', wrt='dens')
+                self.declare_partials(of='mass', wrt='radius')
+
+                self.declare_partials(of='S', wrt='radius')
+
+            def compute(self, inputs, outputs):
+                radius = inputs['radius']
+                dens = inputs['dens']
+
+                outputs['mass'] = (4/3.) * dens * np.pi * radius ** 3
+                outputs['S'] = np.pi * radius ** 2
+
+            def compute_partials(self, inputs, partials):
+                radius = inputs['radius']
+                dens = inputs['dens']
+
+                partials['mass', 'dens'] = (4/3.) * np.pi * radius ** 3
+                partials['mass', 'radius'] = 4. * dens * np.pi * radius ** 2
+
+                partials['S', 'radius'] = 2 * np.pi * radius
+
+        #############################################
+        # Build the ODE class
+        #############################################
+        class CannonballODE(om.ExplicitComponent):
+            """
+            Cannonball ODE assuming flat earth and accounting for air resistance
+            """
+
+            def initialize(self):
+                self.options.declare('num_nodes', types=int)
+
+            def setup(self):
+                nn = self.options['num_nodes']
+
+                # static parameters
+                self.add_input('m', units='kg')
+                self.add_input('S', units='m**2')
+                # 0.5 good assumption for a sphere
+                self.add_input('CD', 0.5)
+
+                # time varying inputs
+                self.add_input('h', units='m', shape=nn)
+                self.add_input('v', units='m/s', shape=nn)
+                self.add_input('gam', units='rad', shape=nn)
+
+                # state rates
+                self.add_output('v_dot', shape=nn, units='m/s**2', tags=['dymos.state_rate_source:v'])
+                self.add_output('gam_dot', shape=nn, units='rad/s', tags=['dymos.state_rate_source:gam'])
+                self.add_output('h_dot', shape=nn, units='m/s', tags=['dymos.state_rate_source:h'])
+                self.add_output('r_dot', shape=nn, units='m/s', tags=['dymos.state_rate_source:r'])
+                self.add_output('ke', shape=nn, units='J')
+
+                # Ask OpenMDAO to compute the partial derivatives using complex-step
+                # with a partial coloring algorithm for improved performance, and use
+                # a graph coloring algorithm to automatically detect the sparsity pattern.
+                self.declare_coloring(wrt='*', method='cs')
+
+                alt_data = USatm1976Data.alt * om.unit_conversion('ft', 'm')[0]
+                rho_data = USatm1976Data.rho * om.unit_conversion('slug/ft**3', 'kg/m**3')[0]
+                self.rho_interp = interp1d(np.array(alt_data, dtype=complex),
+                                           np.array(rho_data, dtype=complex),
+                                           kind='linear')
+
+            def compute(self, inputs, outputs):
+
+                gam = inputs['gam']
+                v = inputs['v']
+                h = inputs['h']
+                m = inputs['m']
+                S = inputs['S']
+                CD = inputs['CD']
+
+                GRAVITY = 9.80665  # m/s**2
+
+                # handle complex-step gracefully from the interpolant
+                if np.iscomplexobj(h):
+                    rho = self.rho_interp(inputs['h'])
+                else:
+                    rho = self.rho_interp(inputs['h']).real
+
+                q = 0.5*rho*inputs['v']**2
+                qS = q * S
+                D = qS * CD
+                cgam = np.cos(gam)
+                sgam = np.sin(gam)
+                outputs['v_dot'] = - D/m-GRAVITY*sgam
+                outputs['gam_dot'] = -(GRAVITY/v)*cgam
+                outputs['h_dot'] = v*sgam
+                outputs['r_dot'] = v*cgam
+                outputs['ke'] = 0.5*m*v**2
+
+        #############################################
+        # Setup the Dymos problem
+        #############################################
+
+        p = om.Problem(model=om.Group())
+
+        p.driver = om.pyOptSparseDriver()
+        p.driver.options['optimizer'] = 'IPOPT'
+        p.driver.declare_coloring()
+
+        p.driver.opt_settings['derivative_test'] = 'first-order'
+        p.driver.opt_settings['mu_strategy'] = 'monotone'
+        p.driver.opt_settings['alpha_for_y'] = 'safer-min-dual-infeas'
+        p.driver.opt_settings['bound_mult_init_method'] = 'mu-based'
+        p.driver.opt_settings['mu_init'] = 0.01
+        p.driver.opt_settings['nlp_scaling_method'] = 'gradient-based'
+
+        p.set_solver_print(level=0, depth=99)
+
+        p.model.add_subsystem('size_comp', CannonballSizeComp(),
+                              promotes_inputs=['radius', 'dens'])
+        p.model.set_input_defaults('dens', val=7.87, units='g/cm**3')
+        p.model.add_design_var('radius', lower=0.01, upper=0.10,
+                               ref0=0.01, ref=0.10, units='m')
+
+        traj = p.model.add_subsystem('traj', dm.Trajectory())
+
+        transcription = dm.Radau(num_segments=25, order=3, compressed=False)
+        phase = dm.Phase(ode_class=CannonballODE, transcription=transcription)
+
+        phase = traj.add_phase('phase', phase)
+
+        # All initial states except flight path angle are fixed
+        # The output of the ODE which provides the rate source for each state
+        # is obtained from the tags used on those outputs in the ODE.
+        # The units of the states are automatically inferred by multiplying the units
+        # of those rates by the time units.
+        phase.set_time_options(fix_initial=True, duration_bounds=(1, 100), units='s')
+        phase.add_state('r', fix_initial=True, solve_segments='forward')
+        phase.add_state('h', fix_initial=True, solve_segments='forward')
+        phase.add_state('gam', fix_initial=False, solve_segments='forward')
+        phase.add_state('v', fix_initial=False, solve_segments='forward')
+
+        phase.add_parameter('S', units='m**2', static_target=True)
+        phase.add_parameter('m', units='kg', static_target=True)
+        phase.add_parameter('CD', val=0.5, opt=False, static_target=True)
+
+        phase.add_boundary_constraint('ke', loc='initial',
+                                      upper=400000, lower=0, ref=100000)
+
+        # A duration balance is added setting altitude to zero.
+        # A nonlinear solver is used to find the duration of required to satisfy the condition.
+        # The duration was bounded to be greater than 1 to ensure the solver did not
+        # converge to the initial point.
+        phase.set_duration_balance('h', val=0.0)
+
+        phase.add_objective('r', loc='final', scaler=-1.0)
+
+        p.model.connect('size_comp.mass', 'traj.phase.parameters:m')
+        p.model.connect('size_comp.S', 'traj.phase.parameters:S')
+
+        # Finish Problem Setup
+        p.setup()
+
+        #############################################
+        # Set constants and initial guesses
+        #############################################
+        p.set_val('radius', 0.05, units='m')
+        p.set_val('dens', 7.87, units='g/cm**3')
+
+        p.set_val('traj.phase.parameters:CD', 0.5)
+
+        guess = initial_guess(t_dur=30.0)
+
+        p.set_val('traj.phase.t_initial', 0.0)
+        p.set_val('traj.phase.t_duration', 30.0)
+
+        p.set_val('traj.phase.states:r', phase.interp('r', ys=guess['r'], xs=guess['t']))
+        p.set_val('traj.phase.states:h', phase.interp('h', ys=guess['h'], xs=guess['t']))
+        p.set_val('traj.phase.states:v', phase.interp('v', ys=guess['v'], xs=guess['t']))
+        p.set_val('traj.phase.states:gam', phase.interp('gam', ys=guess['gam'], xs=guess['t']), units='rad')
+
+        #####################################################
+        # Run the optimization and final explicit simulation
+        #####################################################
+        dm.run_problem(p)
+
+        assert_near_equal(p.get_val('traj.phase.states:r')[-1],
+                          3183.25, tolerance=1.0)
+
+        exp_out = traj.simulate()
+
+        #############################################
+        # Plot the results
+        #############################################
+        rad = p.get_val('radius', units='m')[0]
+        print(f'optimal radius: {rad} m ')
+        mass = p.get_val('size_comp.mass', units='kg')[0]
+        print(f'cannonball mass: {mass} kg ')
+        angle = p.get_val('traj.phase.timeseries.states:gam', units='deg')[0, 0]
+        print(f'launch angle: {angle} deg')
+        max_range = p.get_val('traj.phase.timeseries.states:r')[-1, 0]
+        print(f'maximum range: {max_range} m')
+
+        fig, axes = plt.subplots(nrows=1, ncols=1, figsize=(10, 6))
+
+        time_imp = p.get_val('traj.phase.timeseries.time')
+
+        time_exp = exp_out.get_val('traj.phase.timeseries.time')
+
+        r_imp = p.get_val('traj.phase.timeseries.states:r')
+
+        r_exp = exp_out.get_val('traj.phase.timeseries.states:r')
+
+        h_imp = p.get_val('traj.phase.timeseries.states:h')
+
+        h_exp = exp_out.get_val('traj.phase.timeseries.states:h')
+
+        axes.plot(r_imp, h_imp, 'bo')
+
+        axes.plot(r_exp, h_exp, 'b--')
+
+        axes.set_xlabel('range (m)')
+        axes.set_ylabel('altitude (m)')
+
+        fig, axes = plt.subplots(nrows=4, ncols=1, figsize=(10, 6))
+        states = ['r', 'h', 'v', 'gam']
+        for i, state in enumerate(states):
+            x_imp = p.get_val(f'traj.phase.timeseries.states:{state}')
+
+            x_exp = exp_out.get_val(f'traj.phase.timeseries.states:{state}')
+
+            axes[i].set_ylabel(state)
+
+            axes[i].plot(time_imp, x_imp, 'bo')
+            axes[i].plot(time_exp, x_exp, 'b--')
+
+        plt.show()
+
+
+if __name__ == '__main__':  # pragma: no cover
+    unittest.main()

dymos/phase/options.py

@@ -573,6 +573,9 @@ def __init__(self, read_only=False):
         self.declare(name='t_duration_targets', allow_none=True, default=[],
                      desc='targets in the ODE to which the total duration of the phase is connected')
 
+        self.declare(name='t_duration_balance_options', default={},
+                     desc='options dictionary for the duration residual')
+
 
 class GridRefinementOptionsDictionary(om.OptionsDictionary):
     """