Back to results

Massachusetts Institute of Technology

Real-time quasi-analytical trajectory generation for docking with tumbling objects

Abstract

dc:description.abstract

The capability to rendezvous and dock with tumbling objects has become prominent with increased interest in active debris removal, satellite servicing, and in-space assembly. Guidance and control algorithms have been developed in the literature to allow for a spacecraft to capture an uncooperative and tumbling object under several constraints such as collision avoidance, speed bounds, and thruster saturation. However, current algorithms for this capability do not address plume impingement due to thrusters, which can lead to damage to the target object, and can require the use of nonlinear solvers that neither guarantee convergence of a solution nor be deployed in real-time using current computational capabilities of spacecraft. This thesis presents a quasi-analytical guidance algorithm that allows for a spacecraft to soft-dock with a target, avoids plume impingement, and allows for real-time generation of trajectories with low computational expense. Several test cases compare the solution from this algorithm against a solution using pseudospectral methods and show similar performance at less than 0.1% computational cost, and an example scenario for docking with the the European Space Agency's ENVISAT is presented. Additionally, a discrete transport trajectory optimizer is presented for use as a first cut solution to transporting several components to the same halo orbit for in-space assembly.

Degree

thesis:*
Name thesis:degree_name
Master
Department dc:contributor.department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Grantor dc:publisher
Massachusetts Institute of Technology
Year dc:date.issued
2020

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Cabrales Hernandez, Alejandro D.
Advisor dc:contributor.advisor
  • David W. Miller.

Subjects

dc:subject × 1

Rights

dc:rights
Statement dc:rights
  • MIT theses may be protected by copyright. Please reuse MIT thesis content according to the MIT Libraries Permissions Policy, which is available through the URL provided.
Language dc:language.iso
eng

Identifiers

dc:identifier.*
Handle dc:identifier.uri
https://hdl.handle.net/1721.1/127072
OAI identifier oai:identifier
oai:dspace.mit.edu:1721.1/127072

Chain of custody

source
Harvested from
MIT
Base URL
dspace.mit.edu/oai/request
Last updated
2026-07-22
Source record
OAI-PMH GetRecord
citation

Cabrales Hernandez, Alejandro D.. Real-time quasi-analytical trajectory generation for docking with tumbling objects. Massachusetts Institute of Technology, 2020. https://hdl.handle.net/1721.1/127072