Algorithms of Constructing the Regions of Initial States for Unmanned Winged Gliders

Grumondz, V. T.; Karpezhnikov, E. I.; Polishchuk, M. A.; Полищук, М. В.

doi:10.3103/s1068799817040092

Russ. Aeronaut.

2017

DOI: 10.3103/s1068799817040092

|View full text |Cite

Algorithms of Constructing the Regions of Initial States for Unmanned Winged Gliders

V. T. Grumondz

E. I. Karpezhnikov²,

M. A. Polishchuk

et al.

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...

Citation Types

Supporting

Mentioning

Contrasting

Year Published

2018

2021

Publication Types

Select...

Article2

Relationship

Self Cite0

Independent2

Authors

Journals

Cited by 2 publications

References 1 publication

Supporting

Mentioning

Contrasting

Order By: Relevance

Optimum Control of a Group of Unmanned Gliding Aircraft

Grumondz

Karpezhnikov²

2021

HoBMSTU.SME

View full text Add to dashboard Cite

The paper focuses on an algorithm for controlling a group of unmanned gliding aircraft which are notable for the absence of a propulsion system. The flight is accomplished by using the full mechanical energy reserve received by the unmanned gliding aircraft at the time of the air launch. The task of a group flight with each gliding device being autonomous is currently relevant. Developing a group control algorithm and forming the trajectory of each unmanned gliding aircraft make it possible to solve a wide range of practical problems. This paper states the problem implying the maximization of the flight range with boundary conditions set at the ends of the trajectory. The trajectory of each of the group unmanned gliding aircraft is formed by specifying a reference function for each phase coordinate (xg, yg, zg). The flight range of the group is maximized as a result of solving a boundary value problem by the Ritz --- Galerkin method based on optimization of a function of several variables. In contrast to classical optimization methods, it allows solving the considered optimization problem with sufficient accuracy in a practical sense, without requiring large computational resources for its implementation. This method was used to optimize flight trajectories; however, in this work, it is applied with a number of significant differences both in terms of the problem statement and in terms of requirements for the dynamic capabilities of the aircraft

show abstract

Optimum Control of a Group of Unmanned Gliding Aircraft

Grumondz

Karpezhnikov²

2021

HoBMSTU.SME

View full text Add to dashboard Cite

show abstract

Influence of Interference Effects of the Rotor on the Launch Dynamics of Gliding Unmanned Aerial Vehicle

2018

View full text Add to dashboard Cite

scite is a Brooklyn-based organization that helps researchers better discover and understand research articles through Smart Citations–citations that display the context of the citation and describe whether the article provides supporting or contrasting evidence. scite is used by students and researchers from around the world and is funded in part by the National Science Foundation and the National Institute on Drug Abuse of the National Institutes of Health.

Contact Info

customersupport@researchsolutions.com

10624 S. Eastern Ave., Ste. A-614

Henderson, NV 89052, USA

This site is protected by reCAPTCHA and the Google Privacy Policy and Terms of Service apply.

Blog Terms and Conditions API Terms Privacy Policy Contact Cookie Preferences Do Not Sell or Share My Personal Information

Made with 💙 for researchers

Part of the Research Solutions Family.

Algorithms of Constructing the Regions of Initial States for Unmanned Winged Gliders

Cited by 2 publications

References 1 publication

Optimum Control of a Group of Unmanned Gliding Aircraft

Optimum Control of a Group of Unmanned Gliding Aircraft

Influence of Interference Effects of the Rotor on the Launch Dynamics of Gliding Unmanned Aerial Vehicle

Contact Info

Product

Resources

About