Fari, Stefano and Grande, Davide (2021) Vector Field-based Guidance Development for Launch Vehicle Re-entry via Actuated Parafoil. In: Proceedings of the International Astronautical Congress, IAC. 72th International Astronautical Congress, 2021-10-25 - 2021-10-29, Dubai, United Arab Emirates. ISSN 0074-1795.
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Official URL: https://iafastro.directory/iac/paper/id/66968/summary/
Abstract
In this paper, a launch vehicles re-entry strategy using an actuated parafoil is analyzed. In recent years, this concept is gaining new momentum: it offers a lightweight and cost-effective control solution for autonomous landing of reusable rockets to specific ground or sea coordinates, as well as for mid-air capturing. This landing maneuver requires appropriate modeling together with suitable guidance and control strategies. This work expands upon the following aspects: (1) the development of suitable models for control synthesis and verification; (2) the design of heading control system; (3) the application of a path-following guidance law capable of steering the payload (i.e. the launch vehicle) to the prescribed end-of-mission point. Three models of increasing complexity are proposed based on different assumptions and the dynamics are compared in an ad-hoc simulation environment. MATLAB-Simulink is employed to design two versions of a 6 Degrees Of Freedom (DOF) model accounting for distinct aerodynamic effects. On the other hand, the multi-physics object-oriented language Modelica is used to develop a higher-fidelity 9DOF dynamic model of the system. The latter is then compiled and embedded within MATLAB-Simulink. The same environment allows the implementation of the designed Guidance and Control (G&C) algorithms. The G&C architecture comprises both low-level control loops, regulating course andyaw angles by means of differential steering commands onto the canopy strings, and a guidance layer where the VF path-following is employed. VF methods have already shown remarkable results for fixed-wing unmanned vehicles due to the lower steady-state errors as compared to other approaches, while retaining the potential for real-time implementation. With this work, the method is extended to the application of a launcher recovery. The results of the simulations are investigated, highlighting overall satisfactory performance even in presence of wind disturbances.
Item URL in elib: | https://elib.dlr.de/145123/ | ||||||||||||
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Document Type: | Conference or Workshop Item (Speech) | ||||||||||||
Title: | Vector Field-based Guidance Development for Launch Vehicle Re-entry via Actuated Parafoil | ||||||||||||
Authors: |
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Date: | 25 October 2021 | ||||||||||||
Journal or Publication Title: | Proceedings of the International Astronautical Congress, IAC | ||||||||||||
Refereed publication: | No | ||||||||||||
Open Access: | Yes | ||||||||||||
Gold Open Access: | No | ||||||||||||
In SCOPUS: | Yes | ||||||||||||
In ISI Web of Science: | No | ||||||||||||
ISSN: | 0074-1795 | ||||||||||||
Status: | Published | ||||||||||||
Keywords: | Launch vehicle re-entry, Parafoil, Vector Field path-following, Modelica, Multi-body modeling | ||||||||||||
Event Title: | 72th International Astronautical Congress | ||||||||||||
Event Location: | Dubai, United Arab Emirates | ||||||||||||
Event Type: | international Conference | ||||||||||||
Event Start Date: | 25 October 2021 | ||||||||||||
Event End Date: | 29 October 2021 | ||||||||||||
Organizer: | International Astronautical Federation | ||||||||||||
HGF - Research field: | Aeronautics, Space and Transport | ||||||||||||
HGF - Program: | Space | ||||||||||||
HGF - Program Themes: | Space Transportation | ||||||||||||
DLR - Research area: | Raumfahrt | ||||||||||||
DLR - Program: | R RP - Space Transportation | ||||||||||||
DLR - Research theme (Project): | R - Reusable Space Systems and Propulsion Technology | ||||||||||||
Location: | Bremen | ||||||||||||
Institutes and Institutions: | Institute of Space Systems > Navigation and Control Systems | ||||||||||||
Deposited By: | Fari, Stefano | ||||||||||||
Deposited On: | 03 Nov 2021 09:25 | ||||||||||||
Last Modified: | 23 Oct 2024 08:51 |
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