def testDualServoMargin(self):
control_limits = flap_limits.FlapsToServos(
flap_limits.GetControlLimits())
servo_limits = flap_limits.GetAvionicsServoLimits()
half_degree = math.radians(0.5)
# Shrink servo limits by half a degree on each side.
for servo in ['E1', 'E2', 'R1', 'R2']:
servo_limits[servo] = (servo_limits[servo][0] + half_degree,
servo_limits[servo][1] - half_degree)
self._AssertLimitsContain(servo_limits, control_limits)
def testControlManualLimitsInsideControlLimits(self):
self._AssertLimitsContain(flap_limits.GetControlLimits(),
flap_limits.GetControlManualLimits())
def testControlLimitsInsideSimLimits(self):
self._AssertLimitsContain(
flap_limits.GetSimLimits(),
flap_limits.FlapsToServos(flap_limits.GetControlLimits()))
def testControlCrosswindFlareLimitsInsideControlLimits(self):
self._AssertLimitsContain(flap_limits.GetControlLimits(),
flap_limits.GetControlCrosswindFlareLimits())