Abstract

Autonomy is becoming increasingly important for the robotic exploration of unpredictable environments. One such example is the approach, proximity operation, and surface exploration of small bodies. In this article, we present an overview of an estimation framework to approach and land on small bodies as a key functional capability for an autonomous small-body explorer. We use a multi-phase perception/estimation pipeline with interconnected and overlapping measurements and algorithms to characterize and reach the body, from millions of kilometers down to its surface. We consider a notional spacecraft design that operates across all phases from approach to landing and to maneuvering on the surface of the microgravity body. This SmallSat design makes accommodations to simplify autonomous surface operations. The estimation pipeline combines state-of-the-art techniques with new approaches to estimating the target’s unknown properties across all phases. Centroid and light-curve algorithms estimate the body–spacecraft relative trajectory and rotation, respectively, using a priori knowledge of the initial relative orbit. A new shape-from-silhouette algorithm estimates the pole (i.e., rotation axis) and the initial visual hull that seeds subsequent feature tracking as the body gets more resolved in the narrow field-of-view imager. Feature tracking refines the pole orientation and shape of the body for estimating initial gravity to enable safe close approach. A coarse-shape reconstruction algorithm is used to identify initial landable regions whose hazardous nature would subsequently be assessed by dense 3D reconstruction. Slope stability, thermal, occlusion, and terra-mechanical hazards would be assessed on densely reconstructed regions and continually refined prior to landing. We simulated a mission scenario for approaching a hypothetical small body whose motion and shape were unknown a priori, starting from thousands of kilometers down to 20 km. Results indicate the feasibility of recovering the relative body motion and shape solely relying on onboard measurements and estimates with their associated uncertainties and without human input. Current work continues to mature and characterize the algorithms for the last phases of the estimation framework to land on the surface.

Highlights

  • Autonomy is the ability of a system to achieve goals while operating independently of external control (Fong et al, 2018)

  • We argue that autonomy is enabling for small-body missions because it would allow access to more diverse and remote bodies than the ground-in-the-loop exploration paradigm and would scale to missions that require multiple spacecraft2

  • We used a preplanned spacecraft trajectory and produced trajectory corrections based on estimates and uncertainties that were computed at the different phases

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Summary

INTRODUCTION

Autonomy is the ability of a system to achieve goals while operating independently of external control (Fong et al, 2018). The abundance and diversity (both in the composition and the origin) of small bodies drive the need for greater access, which would require more capable and affordable spacecraft (with higher ΔV) and autonomous operations to reach, approach, land, move, and sample their surface and subsurface. We argue that NEOs are well-suited targets for advancing autonomy, with feed-forward potential to the more challenging outer solar system destinations, including the unknown surfaces of ocean worlds. We argue that autonomy is enabling for small-body missions because it would allow access to more diverse and remote bodies than the ground-in-the-loop exploration paradigm and would scale to missions that require multiple spacecraft. An integrated estimation framework to enable the autonomous approach toward, rendezvous with, and eventual landing on small unexplored bodies. We conclude with an assessment of the viability of the estimation process in establishing situational awareness and share plans for future development

RELATED WORK
Small-Body Cruise and Flyby Operations
Small-Body Proximity Operations
STATE OF THE PRACTICE
Assumptions
Multi-Phase Estimation Framework
Determining Relative Orbits
Estimating the Body Centroid
Feature Tracking
Establishing a Coarse Shape
4.10 Refining the Shape for Selecting Viable Landing Sites
4.11 Identifying Candidate Landing Sites
Notional Spacecraft Architecture
High-Fidelity Mission-Data Generation
Results and Discussion
References frame
CONCLUSION
Full Text
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