seyyed ali saadatdar arani

In this paper, the process of designing and construction of three-drive laboratory Drone system with cold gas thrusters as well as modeling and estimation of its model parameters are presented. These three thrusters are designed with an angle difference of 120 degrees to control the pitch and roll angles. According to the structure of the designed platform, a three-inputs-two-outputs linear model is considered for modeling the mentioned system, and all connections between inputs and outputs are second-order linear models. The parameters of the model have been extracted based on the collection of laboratory data and the use of genetic algorithm. The results obtained from the simulation based on the extracted model and the comparison with the results of the practical tests indicate that a suitable modeling and estimation of the system has been provided. The results show that there is 16% error for modeling and estimation around the roll axis and 19% around the vertical axis, so the estimation around the roll axis is better.

Studies are currently being conducted around the world to realize advanced air Mobility. Advanced Air Mobility is expected to solve various regional issues and provide people with new forms of air transportation. In this article, air travel is investigated as a significant option for improving transportation networks within and between different cities and regions in Iran, and Iran's market profile for accepting Advanced Air Mobility is investigated. Also, the challenges and issues facing Advanced Air Mobility have been studied, finally, some existing plans for use in various missions of Advanced Air Mobility and future mechanisms and plans for the realization and development of this field in Iran have been proposed.