UAV Flight Restriction Control Based on Battery and Temperature

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Solution Overview

Problem

Unmanned aerial vehicles (UAVs) often operate without considering various factors that affect their performance, leading to potential loss of control or crashes due to mismatches between permitted and capable operations, particularly regarding energy sources and environmental conditions.

Innovation Solution

A system that uses processors to receive and process parameters related to UAV operations, including battery state and environmental conditions, to dynamically impose restrictions on UAV operations, ensuring safe and efficient flight by matching internal states with permitted operations.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If UAV operations are permitted without monitoring internal state parameters, then operational flexibility and ease of operation are improved, but reliability deteriorates due to potential loss of control or crashes from over-discharging

Engineering Contradiction:
Improveoperational flexibilityVSAvoidflight safety
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

The system continuously monitors internal state parameters (battery voltage, temperature, motor current) and provides feedback to dynamically adjust operational restrictions. When parameters indicate deteriorating conditions, the system automatically imposes restrictions to prevent unsafe operations, thus maintaining reliability while allowing flexible operation under safe conditions.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The operational restrictions are not static but dynamically adjusted based on real-time internal state parameters. The system transitions between different operational modes (unrestricted, restricted, emergency) depending on the current state, allowing maximum flexibility when conditions are good while ensuring safety when conditions deteriorate.

Inventive Principle:
Principle #15Dynamics

2Reliability

If operational restrictions are imposed based on internal state parameters, then reliability is improved by preventing unsafe operations, but device complexity increases due to monitoring and processing requirements

Engineering Contradiction:
Improveflight safetyVSAvoidsystem complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The processor performs multiple functions: it controls flight operations, monitors internal state parameters, determines operational restrictions, and manages emergency procedures. By making the processor multi-functional, the patent avoids adding separate dedicated hardware for each function, thus improving reliability without proportionally increasing device complexity.

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

Solution Approach 2:

The system combines parameter monitoring, state determination, and restriction enforcement into a single integrated control process. Rather than separate systems for monitoring battery voltage, temperature, and motor current, all these functions are merged into one unified control architecture that processes multiple parameters simultaneously to determine appropriate operational restrictions.

Inventive Principle:
Principle #5Merging (Combining)

3Measurement precision

If environmental conditions are monitored as proxy for internal state, then measurement precision is improved for certain parameters, but loss of information increases due to indirect measurement

Engineering Contradiction:
Improveenvironmental condition measurementVSAvoidinternal state information
Core Design Contradiction:
Measurement precisionVSLoss of information

Solution Approach 1:

The system performs preliminary direct measurement of critical internal state parameters (battery voltage, temperature, motor current) before relying on environmental condition proxies. This ensures accurate baseline information is obtained directly, while environmental monitoring serves as supplementary verification and extends monitoring capability to parameters that are difficult to measure directly.

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS11899443B2Operational parameter based flight restriction
Publication Date: 2024.02.13 SZ DJI TECH CO LTD
  • US11899443B2 patent drawing
  • US11899443B2 patent drawing
  • US11899443B2 patent drawing

AI summary

A system for operating a vehicle includes a first temperature sensor located at a first location and configured to measure a first temperature; a second temperature sensor located at a second location configured to measure a second temperature; and one or more processors. The one or more processors are individually or collectively configured to receive information regarding the first temperature and/or the second temperature; process the information; and impose a restriction affecting operation of the vehicle based on the processed information.