Satellite Attitude Control Simulator Verification

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Solution Overview

Problem

Current satellite attitude control systems face challenges in accurately predicting and verifying satellite attitude control performance, leading to potential unsafe mode transitions and manual intervention, especially when actual satellite operations deviate from predicted attitudes.

Innovation Solution

A method and apparatus that generate and transmit satellite task execution commands based on simulation results from a satellite attitude control simulator, allowing for real-time comparison and adjustment of commands to ensure operations stay within predetermined ranges, thereby enhancing predictive reliability and reducing manual interventions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If satellite attitude control is verified using a simulator and ground observation post, then predictive capability is improved, but system complexity increases

Engineering Contradiction:
Improvepredictive capabilityVSAvoidsystem complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent combines the simulator and ground observation post into an integrated verification system where the simulator generates predicted attitude data and the ground observation post provides actual measurement data, which are then automatically compared to verify satellite attitude control performance without requiring separate manual analysis processes

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The verification system serves multiple functions: it simulates satellite attitude control, measures actual attitude through ground observation, compares predicted versus actual performance, and provides automated verification - replacing multiple separate tools and processes with a single multi-functional system

Inventive Principle:
Principle #6Universality (Multi-functionality)

2Reliability

If manual intervention is used when satellite deviates from predicted attitude, then operational safety is improved, but operational efficiency deteriorates

Engineering Contradiction:
Improveoperational safetyVSAvoidoperational efficiency
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The system implements automated feedback by continuously comparing actual satellite attitude measurements with predicted attitude data from the simulator. When deviations are detected, the system automatically generates verification results and alerts, eliminating the need for manual monitoring while maintaining safety through systematic comparison and automated response protocols

Inventive Principle:
Principle #23Feedback

Data Source

PatentUS10384809B2Method and apparatus for comparing satellite attitude control performances
Publication Date: 2019.08.20 KOREA AEROSPACE RES INST
  • US10384809B2 patent drawing
  • US10384809B2 patent drawing
  • US10384809B2 patent drawing

AI summary

Provided is a method of comparing satellite attitude control performances, the method including generating, by a controller, a satellite task execution command, receiving, by an input and output (I/O) unit, a result of a simulation performed on a satellite attitude control by a satellite attitude control simulator based on the satellite task execution command, and transmitting, by the I/O unit, the satellite task execution command to a satellite based on the result of the simulation.