-----------------------------------------------------------------Abstract--------------------------------------------------------This work mainly focuses on automatic landing control methods for the jumbo jet. The six degree-of-freedom nonlinear model of Boeing707 has been established, using classical control method, gliding beam guidance law, lateral beam guidance law, autoflare guidance law a...

Guidance and control of aircraft in the landing phase imposes extra pilot work loads, hence application of automatic landing control systems is of great importance. In this study automatic landing control systems are introduced and an optimal landing control system is designed. The control system performance criteria are based on minimum control effort. The designed system is simulated for a tr...

Guidance and control of aircraft in the landing phase imposes extra pilot work loads, hence application of automatic landing control systems is of great importance. In this study automatic landing control systems are introduced and an optimal landing control system is designed. The control system performance criteria are based on minimum control effort. The designed system is simulated for a tr...

The control system of the traditional automatic spreader with complex structure and inconvenient servicing is designed based on MCU, and the new control system is designed based on the embedded system. Based on the analysis of the work process and work principle for the automatic spreader, we put forward the new scheme to improve the design of the control system for traditional spreader and des...

This study presents an investigation and evaluation of the control quality automatic system for UAVs in vertical plane under windy conditions. For operational stages general, landing stage is one high-probability that pose a threat to flight safety, especially at time landing. Therefore, evaluate system, authors investigated parameters during UAV The uses PID controller with optimal selected by...