RLBench/envs/_quadrocopter/quadrotor_dynamics.py
def _integrate_derivatives(self, derivatives, dt):
        """Simple euler integration to determine new states."""
        self.state.pos += dt * derivatives.pos
        self.state.vel += dt * derivatives.vel
        self.state.acc[:] = derivatives.acc

        self.state.R += dt * derivatives.R
        self.state.omega += dt * derivatives.omega
Simple euler integration to determine new states.
Simple euler integration to determine new states.
Simple euler integration to determine new states .
def _integrate_derivatives(self, derivatives, dt):
        self.state.pos += dt * derivatives.pos
        self.state.vel += dt * derivatives.vel
        self.state.acc[:] = derivatives.acc
        self.state.R += dt * derivatives.R
        self.state.omega += dt * derivatives.omega
def _integrate_derivatives ( self , derivatives , dt ) : self . state . pos += dt * derivatives . pos self . state . vel += dt * derivatives . vel self . state . acc [ : ] = derivatives . acc self . state . R += dt * derivatives . R self . state . omega += dt * derivatives . omega
Simple euler integration to determine new states.
Simple euler integration to determine new states .
"""Simple euler integration to determine new states."""
self
derivatives
dt