Low-Thrust Spacecraft Transfer Orbit Program

The transfer orbit program for low-thrust spacecraft serves as a critical tool in modern space mission planning and execution. This complete package includes fully functional MATLAB source code accompanied by comprehensive technical documentation. The implementation features trajectory optimization algorithms that calculate fuel-efficient orbital transfers using continuous low-thrust propulsion systems. Key functions include gravitational modeling, thrust vector optimization, and numerical integration methods for precise orbit propagation. Engineers and researchers can readily utilize this program to achieve enhanced navigation precision, enabling more accurate spacecraft positioning and superior data collection capabilities. The modular code architecture allows for straightforward customization to accommodate specific mission parameters and constraints, making this an adaptable and valuable resource for various space exploration applications. The program incorporates advanced control algorithms that dynamically adjust thrust profiles based on orbital mechanics principles, ensuring optimal transfer trajectories while minimizing propulsion system wear.