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Ningshan Wang

Publications and source records attributed to Ningshan Wang.

4 recordsLinked to original sources

Cornering in the Water: An Investigation of Dolphin Swimming Performance

Marine mammal biomechanics research has focused on straight-line swimming at consistent speeds, resulting in a lack of knowledge about how animals select movement strategies to balance cost vs performance during tasks like cornering. In this work we examine performance, maneuverability and cost tradeoffs for bottlenose dolphins (Tursiops truncatus) during prescribed swimming. During the task, animals completed two straight-line sections of swimming with a cornering event (180-degree turn). Movement kinematics were measured with a biologging tag (speed, orientation, and depth), and used to estimate the path of the animal during cornering events using a dead reckoning approach. A hydrodynamic model was used to estimate thrust power and energetic cost during lap swimming. Three animals performed the same swimming task, but the path, cornering strategy, and speed varied between individuals. From the kinematic analysis, TT02 was the fastest lap swimmer, with the highest average lap speed, along with the largest energetic cost. TT01 selected a strategy that reduced energetic cost by sacrificing task performance; the animal took about 1.5 times longer to finish each lap compared to TT02 (36 s vs 23 s). TT03 swam more slowly than TT02 (28 s vs 23 s), but at a 50% reduction in cost per lap. The improved efficiency seen in TT03's movement strategy was the result of reducing transient costs during the lap. This included selecting cornering trajectories that balanced trade-offs between distance traveled and speed loss during the turn. Results from this work provide new insight into maneuverability and movement strategies that the dolphins adopt to balance performance and cost during movement, and provide new knowledge for the design and control of bio-inspired marine robotic systems.

stat.AP

Geometric Extended State Observer on SE(3) with Fast Finite-Time Stability: Theory and Validation on a Rotorcraft Aerial Vehicle

This article presents an extended state observer for vehicle modeled as a rigid body in three-dimensional translational and rotational motions. The extended state observer is applicable to a rotorcraft aerial vehicle with a fixed plane of rotors, modeled as an under-actuated system on the tangent bundle of the six-dimensional Lie group of rigid body motions, SE(3). The extended state observer is designed to estimate the resultant external disturbance force and disturbance torque acting on the vehicle. It guarantees stable convergence of disturbance estimation errors in finite time when the disturbances are constant and finite time convergence to a bounded neighborhood of zero errors for time-varying disturbances. This extended state observer design is based on a Hölder-continuous fast finite time stable differentiator that is similar to the super-twisting algorithm, to obtain fast convergence. Numerical simulations are conducted to validate the proposed extended state observer. The proposed extended state observer is compared with other existing research to show its advantages. A set of experimental results implementing disturbance rejection control using feedback of disturbance estimates from the extended state observer is also presented.

math.DS

Geometric Active Disturbance Rejection Control of Rotorcraft on $SE(3)$ with Fast Finite-Time Stability

This article presents a tracking control framework enhanced by an extended state observer for a rotorcraft aerial vehicle modeled as a rigid body in three-dimensional translational and rotational motions. The system is considered as an underactuated system on the tangent bundle of the six-dimensional Lie group of rigid body motions, $SE(3)$. The extended state observer is designed to estimate the resultant external disturbance force and disturbance torque acting on the vehicle. It guarantees stable convergence of disturbance estimation errors in finite time when the disturbances are constant and finite time convergence to a bounded neighborhood of zero errors for time-varying disturbances. This extended state observer design is based on a Hölder-continuous fast finite time stable differentiator that is similar to the super-twisting algorithm, to obtain fast convergence. A tracking control scheme that uses the estimated disturbances from extended state observer for disturbance rejection, is designed to achieve fast finite-time stable tracking control. Numerical simulations are conducted to validate the proposed extended state observer and tracking control scheme with disturbance rejection. The proposed extended state observer is compared with other existing research to show its supremacy.

math.OC

Geometric PID-type attitude tracking control on SO(3)

This article develops and proposes a geometric nonlinear proportional-integral-derivative (PID) type tracking control scheme on the Lie group of rigid body rotations, SO(3). Like PD-type attitude tracking control schemes that have been proposed in the past, this PID-type control scheme exhibits almost global asymptotic stability in tracking a desired attitude profile. The stability of this PID-type tracking control scheme is shown using a Lyapunov analysis. A numerical simulation study demonstrates the stability of this tracking control scheme, as well as its robustness to a disturbance torque. In addition, a numerical comparison study shows the effectiveness of the proposed integrator term.

eess.SY