Year: 2024
Type: article
Abstract: The article proposes a method for determining the settings for launches by winged aircraft based on the solution of a differential equations system for the movement of aircraft with stabilizing plumage in a disturbing environment, taking into account meteorological factors for the active (passive) segments and the segment of the warhead deployment, and taking into account the nonlinearity and mutual influence of disturbing factors, as well as geophysical conditions of aircraft launch. The proposed method makes it possible to calculate the settings for each launcher and significantly reduce the time for preparing the settings after data entry, using a system of differential equations, taking into account the ballistics of the aircraft and weighting factors for temperature and wind. The accounting of meteorological, ballistic and geophysical conditions proposed in the article, including the ballistic parameters of the movement of the given aircraft, provides the most complete accounting of all disturbing factors affecting the flight of unmanned aerial vehicles, which are solved by a system of differential equations, and it can significantly improve the accuracy of strike preparation. The methodology for calculating meteorological, ballistic, geodetic factors and the calculation of installations for launching aircraft can be used for advanced multiple launch rocket systems.
Language: English
Topic: Guidance and Control Systems
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: diamond
OpenAlex ID: W4409202187