Skip to main navigation Skip to search Skip to main content

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 → …

Fingerprint

Explore the research topics touched on by this project. These labels are generated based on the underlying awards/grants. Together they form a unique fingerprint.
  • A Reusable Launcher Benchmark with Advanced Recovery Guidance

    Simplicio, P., Marcos, A. & Bennani, S., 5 Apr 2019. 20 p.

    Research output: Contribution to conferenceConference Paperpeer-review

    Open Access
    File
    916 Downloads (Pure)
  • Guidance of Reusable Launchers: Improving Descent and Landing Performance

    Simplicio, P., Marcos, A. & Bennani, S., 5 Aug 2019, In: Journal of Guidance, Control, and Dynamics. 14 p.

    Research output: Contribution to journalArticle (Academic Journal)peer-review

    Open Access
    File
    52 Citations (Scopus)
    1388 Downloads (Pure)
  • New Control Functionalities for Launcher Load Relief in Ascent and Descent Flight

    Simplicio, P., Marcos, A. & Bennani, S., 4 Jul 2099.

    Research output: Contribution to conferenceConference Paperpeer-review

    Open Access
    File
    257 Downloads (Pure)