Simulation Framework for Orbit Propagation and Space Trajectory Visualization
Abolfazl Shirazi, Josu Ceberio, José A. Lozano
Abstract
Abolfazl Shirazi, Josu Ceberio, José A. Lozano
Abstract
In this article, an interactive tool for simulation of satellites dynamics and autonomous spacecraft guidance is presented. Different geopotential models for orbit propagation of Earth-orbiting satellites are provided, which consider earth's gravitational field with various accuracies. The presented software is a 3-D visualization platform for space orbit simulation with analytical capabilities through various modules. Taking advantage of a graphical user interface, it can evaluate, analyze, and illustrate the motion of satellite based on different orbit propagation schemes. Several cases of satellites and autonomous spacecraft in the space rendezvous mission are simulated regarding different propagation models to demonstrate the performance of the application in space mission analysis, ground track visualization, and trajectory optimization. Results are validated by comparing with other state-of-the-art tools, such as AGI Systems Tool Kit.
OpenAlex reports 2 citations for this work. Citation counts describe recorded attention and do not establish research quality.
A contribution statement is not available in the OpenAlex record.
Method details are not available in the OpenAlex metadata.
Findings are not separately available in the OpenAlex metadata.
Limitations are not available in the OpenAlex metadata.
Application details are not available in the OpenAlex metadata.
In this article, an interactive tool for simulation of satellites dynamics and autonomous spacecraft guidance is presented. Different geopotential models for orbit propagation of Earth-orbiting satellites are provided, which consider earth's gravitational field with various accuracies. The presented software is a 3-D visualization platform for space orbit simulation with analytical capabilities through various modules. Taking advantage of a graphical user interface, it can evaluate, analyze, and illustrate the motion of satellite based on different orbit propagation schemes. Several cases of satellites and autonomous spacecraft in the space rendezvous mission are simulated regarding different propagation models to demonstrate the performance of the application in space mission analysis, ground track visualization, and trajectory optimization. Results are validated by comparing with other state-of-the-art tools, such as AGI Systems Tool Kit.
Key concepts: Spacecraft, Trajectory, Rendezvous, Visualization, Computer science, Aerospace engineering, Orbit (dynamics), Satellite