The invention provides a
Modelica language-based rapid
simulation method for whole-
process dynamics of a carrier
rocket, and aims to solve the problem of insufficient model
reusability and adaptability in a traditional
simulation method. By utilizing the object-oriented characteristic of the
Modelica language, the method constructs a comprehensive dynamic model, and the model integrates a plurality of subsystems such as a propulsion
system, a
control system and an aerodynamic model. The method comprises the following specific steps: firstly, constructing an overall model of a carrier
rocket, and defining time-varying parameters to accurately calculate key parameters such as
propellant consumption, rotational
inertia and
centroid position; secondly, the influence of different design parameters on the
rocket performance is analyzed through
simulation, so that potential problems are recognized and solved in advance; and moreover, the simulation result can be analyzed, so that the accuracy and reliability of the model are ensured. The innovation of the invention lies in the
modular design and multi-field collaborative simulation capability, which not only significantly improves the
reusability and adaptability of the model, but also effectively supports the design optimization, task planning and control strategy formulation of the rocket. The method not only reduces the research and development cost, but also accelerates the progress of the
spaceflight technology, and has a wide application prospect.