Backstepping based PID Control Strategy for an Underactuated Aerial Robot

2008 ◽  
Vol 41 (2) ◽  
pp. 15636-15641 ◽  
Author(s):  
Ashfaq Ahmad Mian ◽  
Mian Ilyas Ahmad ◽  
Daobo Wang
Keyword(s):  
Control Strategy ◽  
Pid Control ◽  
Aerial Robot

Control System of Sintering Furnace Based on Lonworks Net

2011 ◽  
Vol 48-49 ◽  
pp. 331-334
Author(s):  
Cheng Long Gong ◽  
Jing Zhuo Wang ◽  
Yuan Feng
Keyword(s):  
Control Strategy ◽  
Pid Control ◽  
Sintering Temperature ◽  
Computer Control ◽  
Network System ◽  
Sintering Process ◽  
Fuzzy Pid Control ◽  
Sintering Time ◽  
Combined Control ◽  
Cooling Speed

This paper introduces a computer control network system which can control sintering process of four PTFE molding furnaces accurately. System in-out signals such as sintering temperature, on-off signals of dial motor and aeration motor were connected to Lonworks via net nodes, and network variables were used to construct a configuration and interlinkage between the net nodes. We chose a combined-control strategy in which On-off control or Fuzzy-control or Fuzzy-PID control strategy were selected automatically, so the needs to sintering time, cooling speed, steady-state precision etc were accurately achieved.

A PID control strategy research of vehicle ABS braking based on slip

2021 ◽  
Author(s):  
Junjie Chen ◽  
Guna Wang ◽  
Chang Zhao ◽  
Jiantong Song
Keyword(s):  
Control Strategy ◽  
Pid Control ◽  
Strategy Research

Modelling and PID Control of a Quadrotor Aerial Robot

2014 ◽  
Vol 903 ◽  
pp. 327-331 ◽  
Author(s):  
Ismail Mohd Khairuddin ◽  
Anwar P.P.A. Majeed ◽  
Ann Lim ◽  
Jessnor Arif M. Jizat ◽  
Abdul Aziz Jaafar
Keyword(s):  
Pid Control ◽  
Pitch Angle ◽  
Pid Controller ◽  
Pd Controller ◽  
Proportional Integral Derivative ◽  
Hovering Flight ◽  
Proportional Integral ◽  
Aircraft Model ◽  
Aerial Robot ◽  
Aerial Vehicle

This paper elucidates the modeling of a + quadrotor configuration aerial vehicle and the design of its attitude and altitude controllers. The aircraft model consists of four fixed pitch angle propeller, each driven by an electric DC motor. The hovering flight of the quadrotor is governed by the Newton-Euler formulation. The attitude and altitude controls of the aircraft were regulated using heuristically tuned (Proportional-Integral-Derivative) PID controller. It was numerically simulated via Simulink that a PID controller was sufficient to bring the aircraft to the required altitude whereas the attitude of the vehicle is adequately controlled by a PD controller.

scholarly journals Microwave energy heating process for cycling fluid medium based on APSO-PID control strategy

2012 ◽  
Vol 14 ◽  
pp. 601-607
Author(s):  
Yang Biao ◽  
Li Wei ◽  
Peng Jin-hui ◽  
Guo Sheng-hui ◽  
Zhang Shi-min
Keyword(s):  
Control Strategy ◽  
Pid Control ◽  
Microwave Energy ◽  
Heating Process ◽  
Fluid Medium
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