Algorithmic Support of the System of Automatic Control of Longitudinal Movement of the Small Unmanned Aerial Vehicle Vertigo

Author(s):  
Artem Nikitin ◽  
Sergii Kochuk ◽  
Sergii Firsov
Author(s):  
Matthew Henchey ◽  
Scott Rosen

In the Department of Defense, unmanned aerial vehicle (UAV) mission planning is typically in the form of a set of pre-defined waypoints and tasks, and results in optimized plans being implemented prior to the beginning of the mission. These include the order of waypoints, assignment of tasks, and assignment of trajectories. One emerging area that has been recently identified in the literature involves frameworks, simulations, and supporting algorithms for dynamic mission planning, which entail re-planning mid-mission based on new information. These frameworks require algorithmic support for flight path and flight time approximations, which can be computationally complex in nature. This article seeks to identify the leading academic algorithms that could support dynamic mission planning and recommendations for future research for how they could be adopted and used in current applications. A survey of emerging UAV mission planning algorithms and academic UAV flight path algorithms is presented, beginning with a taxonomy of the problem space. Next, areas of future research related to current applications are presented.


Author(s):  
К. О. Габуев ◽  
В. О. Гонгало ◽  
Н. А. Кучеренко ◽  
А. И. Шипко

The article deals with the use of unmanned aerial vehicles as in industry in general and as in individual branches. The operation of unmanned aerial vehicles in the agricultural sector is described in more detail. The problems existing for today in this sector, as well as the methods of solving these problems with the help of unmanned technologies are given. The important interrelation between the automatic control system and its integration into unmanned aerial vehicles is explained. Detailed description of the technical component of the drone, as well as the relationship between each link of the technical means of automation. An example of the software through which the unmanned aerial vehicle is controlled is given


Author(s):  
M. S. Galtsova ◽  
◽  
M. S. Ryabinkin ◽  

The problem of navigation of an unmanned aerial vehicle at the landing stage in a complex jamming situation is considered. The aim of the work is to develop the structure as well as software and algorithmic support of navigation and landing complex (NPK), using signals from pseudo-satellites (PS) on board a small-sized unmanned aerial vehicle (UAV). Landing is carried out according to a glide-garden approach, while several configurations of models for the location of pseudo-satellites in close proximity to runway are considered. The characteristics of SS location are known in advance with a high degree of accuracy. Estimation errors of aircraft navigation parameters in a horizontal channel of Strapdown inertial navigation system in the conditions when no PS and when one or two PS being used are found.


Ugol ◽  
2020 ◽  
pp. 22-27
Author(s):  
M.L. Kim ◽  
◽  
V.N. Kosterenko ◽  
L.D. Pevzner ◽  
A.A. Jarigin ◽  
...  

Author(s):  
I. V. Zimchuk ◽  
V. I. Ishchenko ◽  
T. M. Shapar

Unmanned aerial vehicles are by far the most promising military and civilian systems. There is a tendency to increase the efforts of a number of leading countries in the development of unmanned aerial vehicles and their complexes. The mathematical model of any system reflects in one way or another its real properties, including the existing limitations. It has been found that one of the most favorable and efficient methods for constructing mathematical models of automatic control systems is to develop them using transfer functions. In order to solve this problem, the article deals with the composition of the control system of a drone. A mathematical model consisting of the joint design of the unmanned aerial vehicle and its automatic control system has been synthesized. The description of the proposed mathematical model of the system is based on the representation of a linear continuous system by the difference equations obtained using the Tustin relation. The mathematical model proposed in the article can be used for the study of typical aircraft whose course management system is built according to the considered structure. The practical significance of the obtained results is the possibility of applying the developed mathematical model to study the dynamics of the change of state and to set up the system of automatic control of the course of the unmanned aerial vehicle through computer simulation. Prospects for further research in this area are computer simulation of an unmanned aerial vehicle control system and estimation of the accuracy of the mathematical model developed.


2021 ◽  
Vol 336 ◽  
pp. 04006
Author(s):  
Haohan Bei ◽  
Yubo Liu ◽  
Wenhao Li ◽  
Ying Huang

UAV (Unmanned Aerial Vehicle) equipment is novel because of its remote automatic control characteristics, so navigation technology is particularly critical. It is necessary to study and apply UAV technology. This paper first analyzes the UAV navigation technology, then the different types of UAV navigation system, and finally looks forward to the development direction of UAV navigation system, hoping that through this study, we can have a general understanding of the application and development trend of UAV navigation technology, and hope that the relevant research can be further enriched and improved to guide practical application.


2019 ◽  
Vol 0 (20) ◽  
pp. 88-97
Author(s):  
Олександр Васильович Збруцький ◽  
Дмитро Олександрович Горбачек

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