Page 112 - Dynamic Vision for Perception and Control of Motion
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3  Subjects and Subject Classes
            96

                                    2
                               2
                                                  2
                              d T / dt  ˜  /[a ˜  (1 i )] .              (3.28)

                                       2 g
                                                  yN
               With i yN in the range of 0.8 to 0.9, usually, and axle distances between 2 and
            3.5 m for cars, angular accelerations to be expected are in the range from about 6 to
            12 rad/s², that is 350 to 700°/s squared resulting in a build–up of  angular speed of
            about 14 to 28°/s per video cycle time of 40 ms. Inertial sensors will immediately
            measure this crisply way, while image interpretation will be confused initially; this
            is a strong argument in favor of combined inertial/visual dynamic scene interpreta-
            tion. Nature, of course, has discovered these complementarities early and continues
            to use them in vertebrate type vision. Figure 3.21 has shown pitch rate and heave
            motion after a step input in surface elevation in the opposite direction in the top
            two graphs (right-hand part); the response extends over many video cycles (~ 1.5
            seconds, i.e.,  about  35 cycles).  Due to tire softness, the effects of a  positive  or
            negative step input will not be exactly the same, but rather similar, especially with
            respect to duration.
            Pitching and rolling motion due to wheel – ground interaction: A very general
            approach to combined visual/inertial perception in ground vehicle guidance  would
            be to mount linear accelerometers in the vertical direction at each suspension point
            of the (four) wheels and additional angular rate sensors around all body axes. The
            sum of the linear accelerations measured, integrated over time, would yield heave
            motion. Integrals of pairwise sums of accelerometer signals (front vs. rear and left
            vs. right-hand side) would indicate pitch and roll accelerations which could then be
            fused with the rate sensor data for improved reliability. Their integral would be
            available with almost no time delay compared to visual interpretation and could be
            of great help when driving in rough terrain, since at least the high-frequency part of
            the body orientation  would  be  known for  visual interpretation. The (low-
            frequency) drift errors of inertial integrals can be removed by results from visual
            perception.
              Remember the big difference between inertial and visual data interpretation: In-
            ertial data are “lead” signals (measured time derivatives) containing the influence
            of all kinds of perturbations, while visual interpretation relies very much on models
            containing (time-integrated) state variables. In vision, perturbations have to be dis-
            covered “in hindsight” when assumptions made do not show up to be valid (after
            considerable delay time).

            3.4.5.2 Lateral Road Vehicle Guidance

            To demonstrate some dynamic effects of details in  modeling of the behavior of
            road vehicles, the lane change maneuvers with the so-called “bicycle model” (see
            Figure 3.10) of a different order are discussed here. First, let us consider an ideal-
            ized maneuver (completely decoupled translational motion and no rotations). Ap-
            plying a constant lateral acceleration a y  (of, say, 2 m/s²) in a symmetrical positive
            and negative fashion, we look for the time T LC in which one lane width W L of 3.6
            m can be traversed with lateral speed v y  back to zero again at the end. One obtains
                                  T    ˜  W  / a .                       (3.29)
                                       2
                                    LC      L  y
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