Aerial Vehicle Power Reachability Control Using Historical Flight Data

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Existing technologies fail to accurately determine whether a movable platform, particularly logistics aerial vehicles, can reach its destination due to insufficient power energy, leading to potential mission failures and resource wastage.

Innovation Solution

A control method that utilizes historical flight data of similar missions to predict energy consumption and combines it with real-time power data to determine if the vehicle can reach its destination, allowing for accurate control strategies to avoid failure.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If traditional control methods are used without historical flight data, then the control system is simple, but the accuracy of destination reach predictions is insufficient

Engineering Contradiction:
Improvedestination reach prediction accuracyVSAvoidcontrol system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The system performs preliminary actions by collecting and storing historical flight data before actual flight missions. This historical data includes energy consumption patterns, flight parameters, and mission outcomes from previous flights. By having this data prepared in advance, the system can accurately predict destination reachability without adding complex real-time computation requirements during actual flights.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system implements feedback mechanisms by continuously comparing actual flight data with historical flight data to improve prediction accuracy. The control apparatus analyzes the difference between predicted energy consumption based on historical data and actual energy consumption, then uses this feedback to refine future predictions and adjust flight control strategies accordingly.

Inventive Principle:
Principle #23Feedback

2Reliability

If real-time energy monitoring and historical data analysis are implemented, then mission failure is avoided, but energy and computational resources are consumed

Engineering Contradiction:
Improvemission completion reliabilityVSAvoidenergy consumption for control operations
Core Design Contradiction:
ReliabilityVSUse of energy by moving object

Solution Approach 1:

The system applies partial action by selectively analyzing only the most critical flight parameters and historical data points necessary for destination reach prediction, rather than processing all possible flight data. This approach ensures sufficient reliability for mission completion while minimizing the energy and computational resources required for control operations.

Inventive Principle:
Principle #16Partial or excessive action

3Ease of operation

If historical flight data is used for prediction, then appropriate control strategies can be adopted, but data processing time increases

Engineering Contradiction:
Improvecontrol strategy selectionVSAvoiddata processing time
Core Design Contradiction:
Ease of operationVSLoss of time

Solution Approach 1:

The system performs preliminary processing of historical flight data during idle periods or between missions, organizing and pre-analyzing the data so that during actual flight operations, only quick comparisons and predictions are needed. This reduces real-time data processing time while maintaining comprehensive analysis capabilities for control strategy selection.

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS20260086578A1Control method of aerial vehicle, control method of movable platform, and apparatus
Publication Date: 2026.03.26 SZ SHANZHI TECH CO LTD
  • US20260086578A1 patent drawing
  • US20260086578A1 patent drawing
  • US20260086578A1 patent drawing

AI summary

A control method includes obtaining a current mission parameter of a current flight mission and historical flight data of a historical flight mission related to the current mission. The current mission parameter is related to an energy consumption of a current aerial vehicle performing the current flight mission, the historical flight data includes a historical mission parameter and a historical energy consumption in the historical flight mission, and the historical mission parameter is related to an energy consumption of a historical aerial vehicle performing the historical mission. The method further includes obtaining a current remaining power energy of the current aerial vehicle in real time, and determining whether the current aerial vehicle is able to reach a destination of the current flight mission based at least one on the current mission parameter, the historical flight data, and the current remaining power energy, to obtain a determination result.