声明
摘要
Abstract
Table of Contents
1 Introduction
1.1 Controller Design Methodology
1.1.1 PID Controller
1.1.2 Proportional and Integral Parameters
1.1.3 Derivative Parameter
1.2 Model Reference Neural Controller
1.2.1 Plant Neural Net Model
1.2.2 Reference Model
1.2.3 Neural Net Controller
1.3 Project Objective
1.4 Notations and Definitions
2 UAV Modeling
2.1 Mathematical Model
2.2 Modeling Environment and Implementation Algorithm
3 Linear Model Analysis
3.1 Linearization
3.2 System Modes and Stability
3.2.1 Longitudinal System Modes
3.2.2 Latitudinal System Modes
3.3 System Step Response
3.3.1 Longitudinal Transfer Functions and Step Response
3.3.2 Latitudinal Transfer Functions and Step Response
3.4 Linear Model Approximation
3.4.1 Longitudinal Linear Model Approximation
3.4.2 Transfcr Function for Pitch Attitude and Pitch Rate
3.4.3 Transfer Function for Speed
3.4.4 Transfer Function for Elevation
3.4.5 Latitudinal Linear Model Approximation
3.4.6 Transfer Function for Roll Attitude and Roll Rate
3.4.7 Transfer Function for Sideslip Angle
3.4.8 Transfer Function for Heading
4 Linear Controller Design
4.1 Longitudinal Controllers
4.1.1 Pitch Attitude Controller Design
4.1.2 Speed Controller Design using Pitch Attitude
4.1.3 Speed Controller Design Using Throttle
4.1.4 Elevation Controller Design
4.2 Latitudinal Controller Design
4.2.1 Roll Attitude Controller Design
4.2.2 Heading Controller Design
5 Neural Controller Design
5.1 Model Reference Pitch Attitude Neural Controller
5.2 Plant and Controller Neural Net Model
5.3 Reference Model
5.4 Simulation and Training
5.5 PID and Neural Net Controller Comparison
Conclusion
References
Appendix
Acknowledgement
大连理工大学;