Flying Body Reflective Surface Control for Position Privacy

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Solution Overview

Problem

Existing methods for precisely measuring a flying body's position in the sky or space using a reflector allow others to determine its location, raising concerns about privacy and unauthorized tracking.

Innovation Solution

A flying body equipped with a reflector, controller, and anti-reflection section that controls the reflection of laser beams based on its position and observation permissions, preventing reflection in unauthorized areas while allowing reflection in permitted areas.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If a reflector is provided on the flying body to enable precise position measurement, then measurement precision is improved, but the flying body's position becomes accessible to unauthorized observers

Engineering Contradiction:
Improveposition measurement precisionVSAvoidunauthorized tracking
Core Design Contradiction:
Measurement precisionVSObject-affected harmful factors

Solution Approach 1:

The reflector's reflective surface is made dynamically controllable through a rotation section that changes its orientation based on the flying body's position and observation permissions. This dynamic adjustment allows the system to enable or disable reflection functionality in real-time, resolving the contradiction between maintaining measurement precision and preventing unauthorized tracking.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The anti-reflection section selectively controls reflection properties in different spatial directions and conditions. By using a shutter mechanism that can be opened or closed based on location, the system creates local variations in reflectivity - allowing reflection when authorized and blocking it when unauthorized - thus resolving the contradiction between measurement precision and security.

Inventive Principle:
Principle #3Local quality

2Object-affected harmful factors

If a shutter is added to control laser reflection intensity, then position measurement security is improved, but device complexity increases

Engineering Contradiction:
Improveunauthorized measurement preventionVSAvoidreflector system complexity
Core Design Contradiction:
Object-affected harmful factorsVSDevice complexity

Solution Approach 1:

The shutter function is merged with the existing reflector structure, creating an integrated anti-reflection section that combines both components into a unified system. This reduces overall device complexity by eliminating separate control mechanisms while maintaining the security function of preventing unauthorized measurement.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The controller automatically manages the shutter and rotation section based on pre-stored position information and observation permissions, enabling the system to self-regulate reflection control without external intervention. This self-service capability reduces operational complexity while maintaining security functions.

Inventive Principle:
Principle #25Self-service

3Adaptability or versatility

If the reflective surface direction is dynamically controlled, then selective position measurement control is improved, but device complexity and energy consumption increase

Engineering Contradiction:
Improveselective reflection controlVSAvoidrotation control system complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The rotation section serves multiple functions: it controls reflective surface orientation for selective measurement control, works in conjunction with the shutter for enhanced security, and adapts to different flying body positions. This multi-functionality justifies the added complexity by providing versatile control capabilities from a single mechanism.

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

Solution Approach 2:

The controller receives feedback about the flying body's position and observation permissions, then automatically adjusts the rotation section and shutter accordingly. This feedback mechanism enables adaptive control that responds to changing conditions, improving versatility while managing complexity through automated decision-making based on pre-stored authorization data.

Inventive Principle:
Principle #23Feedback

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

Effectively prevents unauthorized measurement of the flying body's position while allowing authorized observers to determine its precise location, enhancing privacy and security.

Implementation Method 1

a reflector 100, a controller 200 and an anti-reflection section 300. The reflector 100 is provided on an aperture with a reflective surface 100c which reflects a radiated laser in a direction from which the laser is radiated

Methodology Applied
Scientific EffectReflection: Reflection

Implementation Method 2

The previously described anti-reflection section may be provided on the aperture of the reflector with a shutter which controls an intensity of the laser that the reflector reflects in accordance with the control signal

Methodology Applied
Scientific EffectAbsorption/Blocking: Absorption (EM radiation)

Implementation Method 3

The previously described anti-reflection section may be provided with a rotation section which controls a direction of the reflective surface of the reflector in accordance with the controls signal

Methodology Applied
Scientific EffectRotation:

Data Source

PatentUS11630207B2Flying body
Publication Date: 2023.04.18 MITSUBISHI HEAVY IND LTD
  • US11630207B2 patent drawing
  • US11630207B2 patent drawing
  • US11630207B2 patent drawing

AI summary

A flying body, which prevents others from measuring precise position of the flying body and allows friends to measure precise position of the flying body, is provided. The flying body (10) is provided with a reflector (100), a controller (300) and an anti-reflection section (200). The reflector (100) is provided with a reflective surface, arranged in an aperture, which reflects a radiated laser. The controller (300) generates a control signal on a basis of a state of the flying body. The anti-reflection section (200) prevents a reflection of the laser by the reflective surface on a basis of the control signal.