scholarly journals ANALYTICAL SYNTHESIS OF FORCED PULSE ELECTRONIC DRIVE CONTROL OF A TRACKING SYSTEM

2018 ◽  
pp. 16-20
Author(s):  
A. S. Abufanas ◽  
A. A. Lobaty ◽  
Y. F. Yacina
Keyword(s):  
Unmanned Aerial Vehicles ◽  
Electric Drive ◽  
Duty Cycle ◽  
Power Source ◽  
Control Law ◽  
Tracking Systems ◽  
Constant Amplitude ◽  
Dc Motors ◽  
Aerial Vehicles ◽  
Analytical Synthesis

The problem of analytical synthesis of a control signal by a linear dynamical system is considered. As an optimization criterion, it is proposed to consider the transition time of the system from the initial state to a given final state. This type of control is called forced, providing the maximum system speed. The principle of solving this problem is considered on the basis of application of uncertain Lagrange multipliers and the Pontryagin maximum principle. Expressions are obtained for the matrix of transitions of the system and the control signal in a vector form.As an example, the electric drive described by the widespread second-order mathematical model is considered to evaluate the efficiency of the proposed method. Qualitative illustrations of the operability of the proposed approach, obtained by modeling in the Mathcad environment, and quantitative characteristics of the change in the input and output signals of the hypothetical control system are presented. It is shown that the use of forced control does not lead to the output of variables characterizing the state of the system, beyond the limits of admissible values.The use of forced control makes it possible to synthesize the control law in the form of a sequence of rectangular pulses of constant amplitude determined by the power source, variable duty cycle and polarity. This approach can be used for the control of DC-type DC motors used in various tracking systems used on unmanned aerial vehicles. Key words: forced control, target function, electric drive, pulse train. The use of forced control makes it possible to synthesize the control law in the form of a sequence of rectangular pulses of constant amplitude determined by the power source, variable duty cycle and polarity. This approach can be used for the control of DC-type DC motors used in various tracking systems used on unmanned aerial vehicles.

scholarly journals Electromagnetic Field Analysis and Design of a Hermetic Interior Permanent Magnet Synchronous Motor with Helical-Grooved Self-Cooling Case for Unmanned Aerial Vehicles

2021 ◽  
Vol 11 (11) ◽  
pp. 4856
Author(s):  
Hae-Sol Lee ◽  
Myeong-Hwan Hwang ◽  
Hyun-Rok Cha
Keyword(s):  
Electromagnetic Field ◽  
Unmanned Aerial Vehicles ◽  
Permanent Magnet ◽  
High Power ◽  
Heat Dissipation ◽  
Power Source ◽  
Flight Duration ◽  
Aerial Vehicles ◽  
Drive Motor ◽  
Interior Permanent Magnet

As unmanned aerial vehicles expand their utilization and coverage, research is in progress to develop low-weight and high-performance motors to efficiently carry out various missions. An electromagnetic field interior permanent magnet (IPM) motor was designed and analyzed in this study that improved the flight performance and flight duration of an unmanned aerial vehicle (UAV). The output power and efficiency of a conventional commercial UAV motor were improved by designing an IPM motor of the same size, providing high power output and high-speed operation by securing high power density, wide speed range, and mechanical stiffness. The cooling performance and efficiency of the drive motor were improved without requiring a separate power source for cooling by introducing the helical-grooved self-cooling case, which has a low heat generation structure. Furthermore, the motor is oil-cooled through rotating power without a separate power source, reducing the weight of the UAV. The heat dissipation characteristics were verified by fabricating a prototype and taking actual measurements to verify the validity of the heat dissipation characteristics. The results of this study are expected to improve the flight duration and performance of UAVs and contribute to the efficiency of the design of a UAV drive motor.

scholarly journals Performance analysis of nonlinear observers applied to the fixed-wing unmanned aerial vehicles flight under decoupled-reduced model

2017 ◽  
Vol 9 (2) ◽  
pp. 111-123 ◽  
Author(s):  
Ricardo P Parada ◽  
A Tadeo Espinoza ◽  
Alejandro E Dzul ◽  
Francisco G Salas
Keyword(s):  
Unmanned Aerial Vehicles ◽  
Flight Control ◽  
Sliding Mode ◽  
Reduced Model ◽  
Control Law ◽  
Extended State ◽  
Nonlinear Observers ◽  
Design And Implementation ◽  
Aerial Vehicles ◽  
Nonlinear Extended State Observer

In this paper, we present the design and implementation of two nonlinear observers: nonlinear extended state observer and sliding mode observer for estimating the pitch, yaw and roll angles and angular rates of a fixed-wing unmanned aerial vehicles system under a decoupled-reduced model in real flight experiments. A backstepping control law is designed for control in a decentralized way for altitude, yaw and roll of the airplane. This scheme allows us to test experimentally the feasibility of using the online estimated data from the observers in flight control, which is useful for increasing the robustness of the control and the safety of flight. Furthermore, a comparative analysis of the performance of both nonlinear observers is conducted.

scholarly journals Distributed Control of Networked Unmanned Aerial Vehicles for Valley Area Coverage

2016 ◽  
Vol 2016 ◽  
pp. 1-12
Author(s):  
Mengji Shi ◽  
Kaiyu Qin
Keyword(s):  
Unmanned Aerial Vehicles ◽  
Distributed Control ◽  
A Priori ◽  
Future Research ◽  
Control Law ◽  
Full Coverage ◽  
Aerial Vehicles ◽  
Crash Avoidance ◽  
Pass Through ◽  
Valley Area

The paper provides a novel cooperative motion scheme for networked Unmanned Aerial Vehicles (UAVs) to fully sweep-cover a priori unknown elongated areas with curved borders, which are termed “valley areas.” The UAVs’ motion is confined between the borders. Different from former research on straight-corridor-sweep-coverage, in each valley area, the width of different portions varies dramatically: the UAVs need to line up across the valley area to achieve full coverage of the widest portions while they can only pass through the narrowest parts one by one in a queue. The UAVs are provided with barrier detection and inter-UAV communication. According to the scheme, a distributed control law has been offered for discrete-time multi-UAV systems, guaranteeing crash avoidance and full coverage while considering the constrained mobility of the UAVs. Regular and extreme simulations are carried out to verify the efficacy and stability of the proposed algorithm. Solutions to U-shaped valley coverage and the case of insufficient UAVs available are discussed with validation simulations. Comparison simulations are conducted with respect to a line-sweep-coverage algorithm developed by a closely related work, and differences in performance are revealed subsequently. Conclusions are drawn with possible directions of future research.

scholarly journals Energy-efficient control of a multi-section supercapacitor power supply of an electric drive

2018 ◽  
Vol 161 ◽  
pp. 02002 ◽  
Author(s):  
Vladimir Mozzhechkov
Keyword(s):  
High Voltage ◽  
Electric Drive ◽  
Power Supply ◽  
Energy Efficient ◽  
Mathematical Formulation ◽  
Power Source ◽  
Power Line ◽  
Control Law ◽  
Control Laws ◽  
Efficient Control

A method for synthesizing the control laws of a multi-section supercapacitor power supply of an electric drive is developed. The synthesized control law for an electric drive realizes the prescribed motion and minimizes the required capacitance of the power source. It is achieved through optimal disconnection and connection to the power line of the drive at designated times of one of the power supply sections. Reduction of the required capacitance of the power supply is achieved through a fuller discharge of some of its sections in motion conditions requiring a low level of electrical voltage and saving high voltage in other sections for the respective motion conditions. A mathematical formulation of the problem and a method of its solution is proposed. An example of the implementation of the proposed method is considered.

Non-linear flight control for unmanned aerial vehicles using adaptive backstepping based on invariant manifolds

2012 ◽  
Vol 227 (1) ◽  
pp. 33-44 ◽  
Author(s):  
Jiaming Zhang ◽  
Qing Li ◽  
Nong Cheng ◽  
Bin Liang
Keyword(s):  
Unmanned Aerial Vehicles ◽  
Invariant Manifolds ◽  
Backstepping Control ◽  
Linear Estimator ◽  
Control Law ◽  
Adaptive Backstepping ◽  
Adaptive Backstepping Control ◽  
Aerial Vehicles ◽  
Non Linear ◽  
Aerodynamic Parameters

A novel adaptive backstepping control scheme based on invariant manifolds for unmanned aerial vehicles in the presence of some uncertainties in the aerodynamic coefficients is presented in this article. This scheme is used for command tracking of the angle of attack, the sideslip angle, and the bank angle of the aircraft. The control law has a modular structure, which consists of a control module and a recently developed non-linear estimator. The estimator is based on invariant manifolds, which allows for prescribed dynamics to be assigned to the estimation error. The adaptive backstepping control law combined with the estimator covers the entire flight envelope and does not require accurate aerodynamic parameters. The stability of the whole closed-loop system is analyzed using the Lyapunov stability theory. The full six-degree-of-freedom non-linear model of a small unmanned aerial vehicle is used to demonstrate the effectiveness of the proposed control law. The numerical simulation result shows that this method can yield satisfying command tracking despite some unknown aerodynamic parameters.

scholarly journals Computationaly Simple Obstacle Avoidance Control Law for Small Unmanned Aerial Vehicles

2015 ◽  
Vol 9 (1) ◽  
pp. 50-56 ◽  
Author(s):  
Jakub Cieśluk ◽  
Zdzisław Gosiewski ◽  
Leszek Ambroziak ◽  
Sławomir Romaniuk
Keyword(s):  
Unmanned Aerial Vehicles ◽  
Obstacle Avoidance ◽  
Imaging System ◽  
Information Source ◽  
Digital Camera ◽  
Control Law ◽  
Simulation Studies ◽  
Aerial Vehicles ◽  
Avoidance Control ◽  
Computational Simplicity

Abstract The investigations of the system which allow to avoid obstacles by the unmanned aerial vehicles (UAV) are presented in the paper. The system is designed to enable the full autonomous UAV flight in an unknown environment. As an information source about obstacles digital camera was used. Developed algorithm uses the existing relations between the imaging system and the parameters read from the UAV autopilot. Synthesis of the proposed obstacle avoidance control law was oriented for computational simplicity. Presented algorithm was checked during simulation studies and in-flight tests.

scholarly journals Alternative power source for Small Unmanned Aerial Vehicles (UAV)

2018 ◽  
Vol 19 (9) ◽  
pp. 152-155
Author(s):  
Piotr Mazur
Keyword(s):  
Unmanned Aerial Vehicles ◽  
Power Source ◽  
Aerial Vehicles ◽  
Alternative Power ◽  
Alternative Sources

The article discusses problems of current and development of new, alternative sources of power used for small unmanned aerial vehicles.

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