most citedSingular Zone in Quadrotor Yaw-Position Feedback Linearization

2 citations · 2 across the 6 of their papers we have counts for

collaborators

6 papers

cs.RO2022

Four-dimensional Gait Surfaces for A Tilt-rotor -- Two Color Map Theorem

Zhe Shen, Yudong Ma, Takeshi Tsuchiya

This article presents the four-dimensional surfaces which instruct the gait plan for a tilt-rotor. The previous gaits analyzed in the tilt-rotor research are inspired by animals; n…

cs.RO2022

Feedback Linearization Based Tracking Control of A Tilt-rotor with Cat-trot Gait Plan

Zhe Shen, Yudong Ma, Takeshi Tsuchiya

With the introduction of the laterally bounded forces, the tilt-rotor gains more flexibility in the controller design. Typical feedback linearization methods utilize all the inputs…

cs.RO2022

Cat-inspired Gaits for A Tilt-rotor -- from Symmetrical to Asymmetrical

Zhe Shen, Takeshi Tsuchiya

Among the tilt-rotors (quadrotors) developed in the last decades, Rylls model with eight inputs (four magnitudes of the thrusts and four tilting angles) attracted great attention.…

eess.SY20212 cited

Singular Zone in Quadrotor Yaw-Position Feedback Linearization

Zhe Shen, Takeshi Tsuchiya

It is well known that the conventional quadrotor is an under-actuated MIMO system. The number of the inputs is less than the degree of freedom. One approach in controlling this non…

eess.SY2021

The Pareto-frontier-based Stiffness of A Controller: Trade-off between Trajectory Plan and Controller Design

Zhe Shen, Takeshi Tsuchiya

Approaching a set goal for a UAV comprises a trajectory plan and a controller design (control after plan problems). The optimal trajectory (reference) is calculated before being tr…

eess.SY2021

A Novel Formula Calculating the Dynamic State Error and Its Application in UAV Tracking Control Problem

Zhe Shen, Takeshi Tsuchiya

This paper gives a novel formula (Copenhagen Limit) to calculate/estimate the dynamic state error of a system without a feedforward signal. Copenhagen Limit is in the form of a lim…