Pitch Attitude Hold Autopilot for YTU EC-001 Fixed-Wing Unmanned Aerial Vehicle

被引：0

作者：

Win, Thanda ^{[1
]}

Nyunt, Hteik Tin Cho ^{[1
]}

Tun, Hla Myo ^{[1
]}

机构：

[1] Yangon Technol Univ, Dept Elect Engn, Yangon, Myanmar

来源：

2019 FIRST INTERNATIONAL SYMPOSIUM ON INSTRUMENTATION, CONTROL, ARTIFICIAL INTELLIGENCE, AND ROBOTICS (ICA-SYMP 2019) | 2019年

关键词：

pitch attitude; fixed-wing; unmanned aerial vehicle; autopilot; longitudinal stability derivative;

D O I：

10.1109/ica-symp.2019.8646286

中图分类号：

TP18 [人工智能理论];

学科分类号：

081104 ; 0812 ; 0835 ; 1405 ;

摘要：

Small aircrafts, Unmanned Aerial Vehicles (UAVs), are playing progressively important roles in military and civilian application around the world. This paper focus on pitch attitude hold autopilot design for YTU-EC 001 UAV. The YTU-EC-001 is Fixed-Wing Unmanned Aerial Vehicle in research of Yangon Technological University. In this paper, mathematical modeling, equation of motion on YTU-EC 001 Fixed-Wing Unmanned Aerial Vehicle and the pitch angle and pitch rate transfer functions are derived. These transfer functions showed that the system is stable by using MATLAB. Then controller for pitch altitude system is designed, based on the state space of linear model of the aircraft. A Proportional Integral-Derivative (PID) controller structure is chosen to achieve the system design requirements. The settling time is less than 2 seconds and overshoot should not exceed 3%.

引用

页码：78 / 81

页数：4

共 43 条

[31] A Comparative Study of Four Feedback Linearization Schemes for Motion Planning of Fixed-Wing Unmanned Aerial Vehicles [J].

Khamseh, Hossein Bonyan ;

Torres, Leonardo A. B. .

JOURNAL OF AEROSPACE TECHNOLOGY AND MANAGEMENT, 2016, 8 (01) :63-72

[32] Control System Architecture for Automatic Recovery of Fixed-Wing Unmanned Aerial Vehicles in a Moving Arrest System [J].

Gryte, Kristoffer ;

Sollie, Martin L. ;

Johansen, Tor Arne .

JOURNAL OF INTELLIGENT & ROBOTIC SYSTEMS, 2021, 103 (04)

[33] Aerodynamic Efficiency and Performance Development in an Electric Powered Fixed Wing Unmanned Aerial Vehicle [J].

Kaynak, Berk ;

Arabul, Ahmet Yigit .

ELECTRIC POWER COMPONENTS AND SYSTEMS, 2023, 51 (07) :724-732

[34] Research on Control Law Design of Fixed Wing Unmanned Aerial Vehicle in Aerobatic Maneuvers [J].

Wang, Maolin ;

Fu, Shenghao ;

Liu, Fei ;

Lv, Renli ;

Yu, Nan .

2022 34TH CHINESE CONTROL AND DECISION CONFERENCE, CCDC, 2022, :4665-4670

[35] Control of a fixed wing unmanned aerial vehicle using a robust fractional order controller [J].

Metekia, Enanwo Wondem ;

Asfaw, Wubshet Ayalew ;

Abdissa, Chala Merga ;

Lemma, Lebsework Negash .

SCIENTIFIC REPORTS, 2025, 15 (01)

[36] Control System Architecture for Automatic Recovery of Fixed-Wing Unmanned Aerial Vehicles in a Moving Arrest System [J].

Kristoffer Gryte ;

Martin L. Sollie ;

Tor Arne Johansen .

Journal of Intelligent & Robotic Systems, 2021, 103

[37] A Predictive Path-Following Approach for Fixed-Wing Unmanned Aerial Vehicles in Presence of Wind Disturbances [J].

Rucco, Alessandro ;

Pedro Aguiar, A. ;

Pereira, Fernando Lobo ;

de Sousa, Joao Borges .

ROBOT 2015: SECOND IBERIAN ROBOTICS CONFERENCE: ADVANCES IN ROBOTICS, VOL 1, 2016, 417 :623-634

[38] Feasibility Analysis of Lift-fan-based V/STOL Application on Fixed-wing Unmanned Aerial Vehicles [J].

Wang Huafei ;

Chen Yong ;

Chen Yuanyuan .

DISCOVERY, INNOVATION AND COMMUNICATION - 5TH CSAA SCIENCE AND TECHNIQUE YOUTH FORUM, 2012, :1-6

[39] Accurate and reliable measurement of wing angle characteristics for fixed-wing unmanned aerial vehicles using 3D point cloud [J].

Liu, Guangshuai ;

Li, Xurui ;

Sun, Si ;

Zhao, Xing ;

Li, Bailin .

MEASUREMENT, 2025, 249

[40] Low-Power Peaking-Free Extended-Observer-Based Pitch Autopilot for Morphing Unmanned Aerial Vehicle [J].

Jung, Seungyun ;

Kim, Youdan .

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2021, 45 (02) :362-371

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