Stacked Stewart Platform Assemblers for Precise In-Space Assembly

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Solution Overview

Problem

Current in-space assembly (iSA) concepts rely on complex deployment mechanisms and long-reach manipulators that are mission-specific and incapable of high-precision manipulation, leading to undesirable dynamic modes and requiring additional mass, which limits their effectiveness in assembling large space structures.

Innovation Solution

A modular and reconfigurable manipulation system architecture using stacked Stewart platforms with control algorithms that enable high-accuracy and high-precision autonomous assembly, including fault detection and correction capabilities, allowing the system to adapt and complete tasks without human intervention.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If complex deployment mechanisms and long-reach manipulators are used for in-space assembly, then the ability to assemble large space structures is improved, but the system mass and device complexity increase significantly

Engineering Contradiction:
Improveability to assemble large space structuresVSAvoidsystem complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The system divides the assembly task into multiple components that can be manufactured separately and deployed independently. The space structure is segmented into modular units that are assembled in-orbit, avoiding the need for a single complex manipulator system. Each module can be handled by simpler, more manageable robotic systems.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent employs nested deployment mechanisms where compact structures are folded or nested within smaller launch vehicle constraints, then deployed to their full operational size in-orbit. This allows large structures to be transported and assembled without requiring proportionally large manipulators during the assembly process.

Inventive Principle:
Principle #7Nested doll (Nesting)

2Adaptability or versatility

If complex deployment mechanisms and long-reach manipulators are used for in-space assembly, then the ability to assemble large space structures is improved, but additional mass is required which creates undesirable dynamic modes

Engineering Contradiction:
Improveability to assemble large space structuresVSAvoidsystem mass
Core Design Contradiction:
Adaptability or versatilityVSWeight of moving object

Solution Approach 1:

By segmenting the structure into deployable modules, the system eliminates the need for heavy long-reach manipulators. Each module can be positioned using lighter, more efficient mechanisms, significantly reducing the overall moving mass while maintaining the capability to assemble large structures.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent employs dynamic deployment mechanisms that transform compact configurations into expanded operational configurations. This allows the system to achieve large assembly capabilities without the permanent mass penalty of fixed long-reach manipulators, as the structure dynamically transitions between compact and expanded states.

Inventive Principle:
Principle #15Dynamics

3Adaptability or versatility

If stacked Stewart platforms are used for manipulation, then six degree-of-freedom movement is achieved, but accuracy and precision for the pose of the top plate deteriorate

Engineering Contradiction:
Improvesix degree-of-freedom movement capabilityVSAvoidpose accuracy and precision
Core Design Contradiction:
Adaptability or versatilityVSMeasurement precision

Solution Approach 1:

The system incorporates feedback mechanisms including sensors and control systems that continuously monitor the position and orientation of each Stewart platform module. This feedback enables real-time correction of positioning errors, maintaining high accuracy and precision despite the complexity of stacked six-degree-of-freedom mechanisms.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The patent replaces purely mechanical positioning systems with hybrid systems that incorporate electronic sensors, actuators, and control algorithms. This substitution allows for more precise control and measurement of the top plate pose, overcoming the inherent accuracy limitations of mechanical stacked Stewart platforms alone.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Data Source

PatentUS11989009B2Modular and reconfigurable assembler system for autonomous in-space assembly
Publication Date: 2024.05.21 UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR NAT AERONAUTICS & SPACE ADMINISTRATION
  • US11989009B2 patent drawing
  • US11989009B2 patent drawing
  • US11989009B2 patent drawing

AI summary

Methods and systems to control stacked hexapod platforms for use as tools, which function with both high accuracy and high precision are provided. In some embodiments, the methods and systems include a convergence of modern control theory, and machine learning. Furthermore, some embodiments provide control algorithms to carry out autonomous in-space assembly operations using assemblers. Some embodiments provide methods and systems which combine long-reach low precision manipulators and smaller, high-precision assembler with interchangeable tools.