Fast and robust trajectory optimization

To support deep space exploration with micro spacecraft, it is essential to design orbits that minimize fuel consumption and enable efficient transitions in deep space. We developed orbit optimization software in collaboration with Associate Professor Naoya Ozaki of JAXA’s Institute of Space and Astronautical Science.
We aim to establish a key foundational technology to support the use of microsatellites in future deep space missions.

Features

• Robust trajectory optimization
  Finding the trajectory with the lowest fuel use using DDP.
  Supports automatic differentiation
• Compatible with deep space exploration beyond the moon.
  Compatible with CR3BP (Circular Restricted Three-Body Problem); expansion to N-body is also anticipated.
• Fast trajectory optimization
  Accelerating Computational Processing with GPUs
• Adjusts to different usage patterns based on the situation.
  We are developing a cloud version that requires no local environment and an installation version for core users.
  (The cloud version will be released on the web soon.)