Reusable Launcher Guidance & Control with Active Load Relief

  • Simplicio, Pedro V M (Principal Investigator)
  • Marcos, Andres (Principal Investigator)

Project Details

Description

The objective of this project is to improve launcher performance via integrated guidance & control design featuring retro-propulsive entry, descent and pinpoint landing, robust control techniques and aerodynamic load relief algorithms.
StatusActive
Effective start/end date1/02/17 → …