V V Markelov's scientific contributions
What is this page?
This page lists the scientific contributions of an author, who either does not have a ResearchGate profile, or has not yet added these contributions to their profile.
It was automatically created by ResearchGate to create a record of this author's body of work. We create such pages to advance our goal of creating and maintaining the most comprehensive scientific repository possible. In doing so, we process publicly available (personal) data relating to the author as a member of the scientific community.
If you're a ResearchGate member, you can follow this page to keep up with this author's work.
If you are this author, and you don't want us to display this page anymore, please let us know.
It was automatically created by ResearchGate to create a record of this author's body of work. We create such pages to advance our goal of creating and maintaining the most comprehensive scientific repository possible. In doing so, we process publicly available (personal) data relating to the author as a member of the scientific community.
If you're a ResearchGate member, you can follow this page to keep up with this author's work.
If you are this author, and you don't want us to display this page anymore, please let us know.
Publications (15)
The provision of the specified accuracy characteristics is one of the main indicators of the functioning of the inertial navigation system (INS) of the aircraft. The accuracy and functional characteristics of INS are determined by the quality of the used measuring sensors: angle rates and accelerations, as well as by the functions of the built-in s...
One of the main trends in the development of modern on-board navigation systems is aimed at increasing the predictability of the aircraft’s flight path in space and time. That in its turn should improve the accuracy of evaluation of fuel and operating costs, improving the quality dispatch services and bandwidth airspace. At the same time, the predi...
The satellite navigation and precision inertial system development quality leap provided a significant increase of the object position definition accuracy characteristics. This technology implementation in aviation led to possibility of flights in the given trajectory coordinates through a geodesy system without application of ground radio beacons...
This article presents the current process of designing automated systems assigned for computer-aided design. The basic mission of constructing such systems depending on the type of design tasks is described. An example of the problem of designing the upper level of the primary look of the aircraft avionics complex is given. The main tasks for which...
The trend of development of modern on-board aircraft systems causes the emergence of new requirements, in particular, to maintain the specified accuracy characteristics while the air navigation. One of these requirements is the implementation of reverse flight schemes, which include standard turns and final turns with the control of the exit to the...
Modern requirements in accuracy of aircraft flight trajectory following is done with specifications to the systems of zone navigation in the international air space RNAV (Area Navigation) and RNP (Required Navigation Performance) may apply tight restrictions for the possibilities to correct for the aircraft arrival time to the points of route. Appl...
The task is being studied to evaluate the amount of quality to perceive the picture elements being projected on LCD screens of modern on-board visual means to display the information. A mean to display information is a multi-functional colorful indicator. The display itself (the frame being displayed) is a sign and symbol information. The symbol pe...
Further increase in airspace capacity and flight efficiency makes it expedient to introduce four-dimensional flight trajectories, as well as operations based on their use, in order to maintain a high level of safety. At the same time, the implementation of control systems that support maintenance of four-dimensional trajectories faces some problems...
Background/Objectives: Development of algorithms for flight plan data transformation into the projected trajectory of the aircraft based on the unification of used trajectories in the horizontal plane to reduce the consumed computing resources. Methods: In order to display the flight route, specialized software is used in the on-board systems enabl...
The use of the correction course option before aircraft take-off after inertial navigation system (INS) inaccurate alignment based on the platform attitude-and-heading reference system in azimuth is considered in the paper. A course correction is performed based on the track angle defined by the information received from the satellite navigation sy...
Subject of Research.We consider the principles and algorithms for construction of en-route flight paths of an aircraft (airplane) in a horizontal plane for their subsequent display on the navigation situation indicators in the cockpit. Navigation situation indicatorsaredisplay devices designed on the basis of flat liquid crystal panel. Methods. Fli...
Citations
... The use of high-precision navigation causes increased requirements for the accuracy of maintaining a given flight trajectory, including turns [7,8]. One of these requirements when performing reverse schemes is the exit to the given path line at the given point, in particular, the exit to the final approach at the given distance from runway end [9,10]. ...
... A calculation method based on the physical principles of the functioning of inertial navigation systems is used as a reference dead reckoning model. The initial data for the reference model are the parameters measured (estimated) by INS [3,4]. The results of the reference model are parameters that include ground speeds and coordinates of the aircraft location, calculated from the initial data, provided that the initial INS alignment at the angles of roll, pitch and heading is correct. ...
