All Stories

  1. Implementing life cycle sustainability assessment for improved space mission design
  2. Multi-Objective Optimisation under Uncertainty with Unscented Temporal Finite Elements
  3. Robust Trajectory Optimisation of a TSTO Spaceplane Using Uncertainty-Based Atmospheric Models
  4. Direct Solution of Multi-Objective Optimal Control Problems Applied to Spaceplane Mission Design
  5. Conceptual design analysis for a two-stage-to-orbit semi-reusable launch system for small satellites
  6. Multi-Objective Optimal Control of Re-entry and Abort Scenarios
  7. Vehicle and Mission Design of a Future Small Payload Launcher
  8. Spaceplane trajectory optimisation with evolutionary-based initialisation
  9. Multi-Objective Optimal Control of the Ascent Trajectories of Launch Vehicles
  10. Global solution of multi-objective optimal control problems with multi agent collaborative search and direct finite elements transcription
  11. Design of a formation of solar pumped lasers for asteroid deflection
  12. Integrated 915 MHz dual-patch circularly polarized antenna for Suaineadh space web experiment
  13. On the deflection of asteroids with mirrors
  14. Mirror Formation Control in the Vicinity of an Asteroid
  15. Design of optimal spacecraft‐asteroid formations through a hybrid global optimization approach
  16. Optimal design for a NEO tracking spacecraft formation
  17. Comparison of Single and Multi-Spacecraft Configurations for NEA Deflection by Solar Sublimation