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Embry Riddle Aeronautical University

Adaptive-Optimal Control of Spacecraft near Asteroids

Abstract

dc:description.abstract

<p>Spacecraft dynamics and control in the vicinity of an asteroid is a challenging and exciting problem. Currently, trajectory tracking near asteroid requires extensive knowledge about the asteroid and constant human intervention to successfully plan and execute proximity operation. This work aims to reduce human dependency of these missions from a guidance and controls perspective. In this work, adaptive control and model predictive control are implemented to generating and tracking obstacle avoidance trajectories in asteroid’s vicinity.</p> <p>Specifically, direct adaptive control derived from simple adaptive control is designed with e modification to track user-generated trajectories in the presence of unknown system and sensor noise. This adaptive control methodology assumes no information on the system dynamics, and it is shown to track trajectories successfully in the vicinity of the asteroid. Then a nonlinear model predictive control methodology is implemented to generate obstacle avoidance trajectories with minimal system information namely mass and angular velocity of the asteroid.</p> <p>Ultimately, the adaptive control system is modified to include feed-forward control input from the nonlinear model predictive control. It is shown through simulations that the new control methodology names direct adaptive model predictive control (DAMPC), is able to generate sub-optimal trajectories. A comparative study is done with Asteroid Bennu, Kleopatra and Eros to show the benefits of DAMPC over adaptive control and MPC. A study on effect of noisy measurements and model is also conducted on adaptive control and direct adaptive model predictive control.</p>

Degree

thesis:*
Name thesis:degree_name
Doctor of Philosophy in Aerospace Engineering
Level thesis:degree_level
Dissertation - Open Access
Discipline thesis:degree_discipline
Aerospace Engineering
Year
2021

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Tiwari, Madhur

Subjects

dc:subject × 5

Identifiers

dc:identifier.*
Repository record dc:identifier
https://commons.erau.edu/edt/619
OAI identifier oai:identifier
oai:commons.erau.edu:edt-1631

Chain of custody

source
Harvested from
Embry Riddle Aeronautical University
Base URL
commons.erau.edu/do/oai/
Last updated
2026-07-27
Source record
OAI-PMH GetRecord
citation

Tiwari, Madhur. Adaptive-Optimal Control of Spacecraft near Asteroids. Dissertation - Open Access thesis, 2021. https://commons.erau.edu/edt/619