Gravity-Turn-Based Precise Landing Guidance for Reusable Rockets

Runqiu Yang, Xinfu Liu*

*Corresponding author for this work

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

3 Citations (Scopus)

Abstract

This paper presents a gravity-turn-based precise landing guidance algorithm for reusable rockets with the consideration of aerodynamic drag and necessary path constraints for operation safety. First, a gravity-turn trajectory is found to make the rocket have a soft landing. Then, to eliminate the downrange and crossrange errors, which is required by precise landing, we propose to solve an optimal control problem to correct the thrust acceleration associated with the gravity-turn trajectory. In the end, we can design an algorithm requiring only solving a one-parameter root-finding problem and a small-scale linear programming problem. Numerical examples are provided to demonstrate the performance of the guidance algorithm.

Original languageEnglish
Title of host publicationAdvances in Guidance, Navigation and Control - Proceedings of 2020 International Conference on Guidance, Navigation and Control, ICGNC 2020
EditorsLiang Yan, Haibin Duan, Xiang Yu
PublisherSpringer Science and Business Media Deutschland GmbH
Pages3423-3434
Number of pages12
ISBN (Print)9789811581540
DOIs
Publication statusPublished - 2022
EventInternational Conference on Guidance, Navigation and Control, ICGNC 2020 - Tianjin, China
Duration: 23 Oct 202025 Oct 2020

Publication series

NameLecture Notes in Electrical Engineering
Volume644 LNEE
ISSN (Print)1876-1100
ISSN (Electronic)1876-1119

Conference

ConferenceInternational Conference on Guidance, Navigation and Control, ICGNC 2020
Country/TerritoryChina
CityTianjin
Period23/10/2025/10/20

Keywords

  • Gravity turn
  • Precise landing guidance
  • Reusable rocket landing

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