Safe Landing on Small Celestial Bodies with Gravitational Uncertainty Using Disturbance Estimation and Control Barrier Functions

Fuente: arXiv
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Main Authors: Arenas-Uribe, Felipe, Seigler, T. Michael, Hoagg, Jesse B.
Format: Preprint
Published: 2025
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author Arenas-Uribe, Felipe
Seigler, T. Michael
Hoagg, Jesse B.
author_facet Arenas-Uribe, Felipe
Seigler, T. Michael
Hoagg, Jesse B.
contents Soft landing on small celestial bodies (SCBs) poses unique challenges, as gravitational models poorly characterize the higher-order gravitational effects of SCBs. Existing control approaches lack guarantees for safety under gravitational uncertainty. This paper proposes a three-stage control architecture that combines disturbance estimation, trajectory tracking, and safety enforcement. An extended high-gain observer estimates gravitational disturbances online, a feedback-linearizing controller tracks a reference trajectory, and a minimum-intervention quadratic program enforces state and input constraints while remaining close to the nominal control. The proposed approach enables aggressive yet safe maneuvers despite gravitational uncertainty. Numerical simulations demonstrate the effectiveness of the controller in achieving soft-landing on irregularly shaped SCBs, highlighting its potential for autonomous SCB missions.
format Preprint
id arxiv_https___arxiv_org_abs_2510_05895
institution arXiv
publishDate 2025
record_format arxiv
spellingShingle Safe Landing on Small Celestial Bodies with Gravitational Uncertainty Using Disturbance Estimation and Control Barrier Functions
Arenas-Uribe, Felipe
Seigler, T. Michael
Hoagg, Jesse B.
Systems and Control
Optimization and Control
70Q05, 93C85, 93C10
Soft landing on small celestial bodies (SCBs) poses unique challenges, as gravitational models poorly characterize the higher-order gravitational effects of SCBs. Existing control approaches lack guarantees for safety under gravitational uncertainty. This paper proposes a three-stage control architecture that combines disturbance estimation, trajectory tracking, and safety enforcement. An extended high-gain observer estimates gravitational disturbances online, a feedback-linearizing controller tracks a reference trajectory, and a minimum-intervention quadratic program enforces state and input constraints while remaining close to the nominal control. The proposed approach enables aggressive yet safe maneuvers despite gravitational uncertainty. Numerical simulations demonstrate the effectiveness of the controller in achieving soft-landing on irregularly shaped SCBs, highlighting its potential for autonomous SCB missions.
title Safe Landing on Small Celestial Bodies with Gravitational Uncertainty Using Disturbance Estimation and Control Barrier Functions
topic Systems and Control
Optimization and Control
70Q05, 93C85, 93C10
url https://arxiv.org/abs/2510.05895