Aircraft Actuator Control with Adaptive Load Limits

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Solution Overview

Problem

Actuator systems in multiactuator aerial vehicles (MAVs) face degradation and overload due to uneven power distribution, as existing methods do not consider the health status and characteristics of individual actuators, leading to overheating and failure.

Innovation Solution

A method for controlling actuator systems that allocates tasks based on a weight matrix and physical control limits, dynamically adjusting these parameters to ensure each actuator operates within its available capacity, preventing overload and degradation by using a computer algorithm to determine and apply new control inputs based on real-time sensor data.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If actuators are allocated tasks without considering health status and characteristics, then task completion is achieved, but actuator degradation and overload occur

Engineering Contradiction:
Improveactuator reliabilityVSAvoidtask completion efficiency
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The patent dynamically adjusts the weight matrix W and physical maximum control limits uimax based on real-time actuator health status and characteristics. By monitoring actuator conditions and modifying these parameters accordingly, the system optimizes task allocation to prevent overload while maintaining effective task completion. This resolves the contradiction by adapting allocation parameters to current actuator states rather than using fixed allocation methods.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent implements continuous monitoring of actuator health status and characteristics, using this feedback to dynamically adjust the weight matrix and control limits. The system repeatedly performs comparisons and updates allocation parameters based on current actuator conditions, creating a closed-loop control system that prevents degradation while maintaining productivity through adaptive reallocation.

Inventive Principle:
Principle #23Feedback

2Speed

If actuators operate at peak power continuously, then task execution speed is improved, but overheating and motor failure occur

Engineering Contradiction:
Improvetask execution speedVSAvoidactuator temperature
Core Design Contradiction:
SpeedVSTemperature

Solution Approach 1:

The patent makes the actuator allocation dynamic by continuously adjusting the weight matrix W and control limits uimax based on real-time actuator temperature and health status. Rather than static allocation, the system adapts allocation parameters dynamically, reducing power demand on overheating actuators while maintaining overall task execution speed through redistribution to healthy actuators.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The patent performs preliminary monitoring of actuator temperature and health status before allocation decisions are made. By detecting early signs of overheating or degradation, the system proactively adjusts the weight matrix and control limits to prevent temperature excursions and motor failure, rather than reacting after damage occurs.

Inventive Principle:
Principle #10Preliminary action

3Reliability

If power demand increases on remaining actuators after failure, then task completion is maintained, but overload cascade and further failures occur

Engineering Contradiction:
Improvesystem reliabilityVSAvoidactuator power demand
Core Design Contradiction:
ReliabilityVSPower

Solution Approach 1:

The patent uses continuous feedback on actuator health status and power demand to dynamically adjust the weight matrix and control limits. When actuator failures or degradation are detected, the system monitors power demand trends and adjusts allocation parameters to prevent excessive power demands that would trigger overload cascades, maintaining system reliability through proactive power management.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The patent implements beforehand cushioning by setting adaptive control limits uimax based on actuator health status and historical performance. These pre-established protective limits prevent power demands from exceeding safe thresholds even when task requirements increase, cushioning the system against overload cascades and further failures before they can occur.

Inventive Principle:
Principle #11Beforehand cushioning (Prior cushioning)

Data Source

PatentUS11720124B2Method of controlling an actuator system and aircraft using said method
Publication Date: 2023.08.08 VOLOCOPTER TECHNOLOGIES GMBH
  • US11720124B2 patent drawing
  • US11720124B2 patent drawing
  • US11720124B2 patent drawing

AI summary

A method of controlling an actuator system including a plurality of k actuators. Each of the actuators-receives a control input ui, wherein index i denotes a particular actuator, which control input ui is determined depending on a weight matrix W including a weighting factor wi for each actuator and depending on at least a physical maximum control limit uimax for each of the actuators. The weighting factors wi and/or physical maximum control limit uimax are actively changed during operation if a first comparison of the control input ui or a function f(ui) thereof with a set first threshold value yields that the control input ui or function f(ui) thereof exceeds the set first threshold value. The first comparison is repeated during operation, and a new control input ui is determined from the adjusted weighting factor wi and/or the adjusted physical maximum control limit uimax and applied to the actuators.