scholarly journals A Practical Trajectory Tracking Scheme for a Twin-Propeller Twin-Hull Unmanned Surface Vehicle

2021 ◽  
Vol 9 (10) ◽  
pp. 1070
Author(s):  
Jiucai Jin ◽  
Deqing Liu ◽  
Dong Wang ◽  
Yi Ma

Trajectory tracking is a basis of motion control for Unmanned Surface Vehicles (USVs), which has been researched well for common USVs. The twin-propeller and twin-hull USV (TPTH-USV) is a special vehicle for applications due to its good stability and high load. We propose a three-layered architecture of trajectory tracking for the TPTH-USV which explicitly decomposes into trajectory guidance, a motion limitator and controller. The trajectory guidance transforms an expected trajectory into an expected speed and expected course in a kinematic layer. The motion limitator describes some restriction for motion features of the USV in the restriction layer, such as the maximum speed and maximum yaw rate. The controller is to control the speed and course of the USV in the kinetic layer. In the first layer, an adaptive line-of-sight guidance law is designed by regulating the speed and course to track a curved line considering the sideslip angle. In the second layer, the motion features are extracted from an identified speed and course coupled model. In the last layer, the course and speed controller are designed based on a twin-PID controller. The feasibility and practicability of the proposed trajectory tracking scheme is validated in sea experiments by a USV called ‘Jiuhang 490’.

2019 ◽  
Vol 175 ◽  
pp. 217-222 ◽  
Author(s):  
Haibin Huang ◽  
Mian Gong ◽  
Yufei Zhuang ◽  
Sanjay Sharma ◽  
Dianguo Xu

2015 ◽  
Vol 645-646 ◽  
pp. 653-656
Author(s):  
Yu Cai ◽  
Wei Xiong ◽  
Xiao Tang Cao ◽  
Zhao Ying Zhou

This paper studies a new trajectory guidance logic system for Bank-To-Turn fixed-wing (BTT) micro air vehicle (MAV) based on MEMS sensor / GPS , and introduce the method of estimating the navigation information from MEMS sensors and GPS. a nonlinear guided logic based on literature is utilized to get the desired roll angle , and a total energy controller is utilized in the longitudinal loop. Based on the kinematic model of the coordinated turning of MAV, the system can ensure that the aircraft stably track a flight plan segment. Flight tests on MAV prove the feasibility of the trajectory guidance logic system.


Electrician ◽  
2021 ◽  
Vol 15 (1) ◽  
pp. 20-24
Author(s):  
Wiwin A Oktaviani ◽  
Ibnu Sukri

In general, the Brushless DC motor speed controller uses an Atmega 16 microcontroller and a MOSFET, which often increases the MOSFET's temperature, especially when the motor is loaded. This article discusses the use of the IC NE555 and CD4017 as a frequency regulator to the MOSFET gate by periodically igniting the forward voltage from the change in the potentiometer value. We carried out the test in an unloaded and unloaded state with voltage variations of 2.5 Vac, 7.5 Vac, 12.5 Vac, and 19.5 Vac. The test results show an excellent tool response where the higher the frequency value, the motor speed will increase. The maximum speed when unloaded reaches rpm at a frequency of 574.6. Whereas in the load test, the full speed reaches 20987 rpm at a frequency of 524.675 Hz. During the test, there was no temperature increase in the MOSFET.  


2000 ◽  
Vol 23 (4) ◽  
pp. 754-756 ◽  
Author(s):  
Craig A. Kluever ◽  
Daniel J. O’Shaughnessy

2015 ◽  
Vol 2015 ◽  
pp. 1-14 ◽  
Author(s):  
Yongwei Zhang ◽  
Min Gao ◽  
Suochang Yang ◽  
Dan Fang

Guidance with traditional trajectory correction scheme usually starts from the trajectory apex time to reduce drag penalties early in flight; however, this method cannot get the max trajectory correction capability of canards according to our analysis. This paper presents an optimized trajectory correction scheme by taking different control phases of canards in ballistic ascending segment and ballistic descending segment. Simulation indicates that the optimized trajectory correction can improve the trajectory correction capability greatly. The result of an example trajectory and Monte Carlo simulations with the predictive guidance law and the trajectory tracking guidance law testifies the effectiveness of the optimized trajectory correction scheme.


Author(s):  
Sen ZHANG ◽  
Chao JIN ◽  
Cui-sheng WU ◽  
Yuan-heng ZHANG ◽  
Ting-ting YANG ◽  
...  

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