BS Rockets

Modern methods of mathematical modeling and numerical analysis are used to calculate the parameters of launch vehicles and spacecraft within small classes of equipment. The work uses flight dynamics modeling, optimization methods, and machine learning algorithms to improve the accuracy of forecasting and control at different stages of the flight. The programming languages ​​C++, Python, Go, MATLAB and other development tools are used, which ensures flexibility of implementation and computational efficiency.

Capabilities include the development and verification of software for control systems, trajectory modeling, stabilization and navigation, as well as simulation of operating conditions under practical implementation conditions. For small spacecraft and satellite constellations, services are provided to create turnkey solutions and customize software for specific tasks, including the integration of various modules, testing under simulation conditions, as well as technical support throughout the project life cycle.

Additionally, work is carried out on analyzing system requirements, designing software architecture, creating prototypes and conducting designated tests. Measures are provided to ensure the reliability and sustainability of systems, including advanced verification and validation methods, as well as security audits and compatibility with existing infrastructure. Clients receive detailed technical specifications, validation plans, operational documentation, and support during the implementation and operation stages.