Unified Aircraft Inceptor With Haptic Feedback for Lower Pilot Workload

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Solution Overview

Problem

Current aircraft control systems require multiple input mechanisms and complex feedback systems, increasing cognitive workload and system complexity, while also being inefficient in terms of mass and ergonomics, especially in varying flight regimes and environments.

Innovation Solution

A unified aircraft control system utilizing a single inceptor with integrated haptic feedback and passive soft stops, allowing for reduced input mechanisms and streamlined feedback, enabling efficient control across different flight modes without the need for direct thumb and finger manipulation, and incorporating an adjustable hand rest for improved ergonomics.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If multiple input mechanisms and complex feedback systems are used, then control precision and reliability are improved, but device complexity and cognitive workload increase

Engineering Contradiction:
Improvecontrol reliabilityVSAvoidsystem complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent combines multiple input mechanisms into a single inceptor device that integrates pitch and roll controls. The inceptor includes a grip portion with integrated control axes, eliminating the need for separate control sticks or wheels while maintaining full control functionality through a unified interface

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The inceptor is designed as a universal control device that performs multiple functions simultaneously - controlling both pitch and roll axes, providing haptic feedback, and supporting various grip configurations. This multi-functional design replaces traditional separate control mechanisms with a single versatile device

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

2Measurement precision

If multiple input mechanisms and complex feedback systems are used, then control precision and reliability are improved, but cognitive workload increases

Engineering Contradiction:
Improvecontrol precisionVSAvoidcognitive workload
Core Design Contradiction:
Measurement precisionVSEase of operation

Solution Approach 1:

The inceptor provides self-service through automatic haptic feedback that guides the operator's hand to the correct neutral position and provides tactile cues for control inputs. The system actively assists the operator rather than requiring complex manual interpretation, reducing cognitive load while maintaining precision

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The inceptor incorporates haptic feedback mechanisms that provide real-time tactile information to the operator about control surface positions and aircraft attitude. This feedback loop enables precise control with minimal cognitive effort by allowing the operator to feel the control state rather than interpreting complex visual or auditory signals

Inventive Principle:
Principle #23Feedback

3Ease of manufacture

If fixed control systems are used, then manufacturing simplicity is improved, but adaptability to different flight regimes deteriorates

Engineering Contradiction:
Improvemanufacturing simplicityVSAvoidflight regime adaptability
Core Design Contradiction:
Ease of manufactureVSAdaptability or versatility

Solution Approach 1:

The inceptor incorporates adjustable components including a movable hand rest that can be repositioned along the grip axis and variable resistance mechanisms that adapt to different flight conditions. These dynamic elements allow the control system to optimize performance across hover, transition, and forward flight regimes without requiring multiple fixed control devices

Inventive Principle:
Principle #15Dynamics

Data Source

PatentUS11673649B2Aircraft control system and method
Publication Date: 2023.06.13 JOBY AERO INC
  • US11673649B2 patent drawing
  • US11673649B2 patent drawing
  • US11673649B2 patent drawing

AI summary

The aircraft control system 100 includes an inceptor with a set of primary inceptor axes and a set of secondary inceptor inputs. The inceptor can optionally include a hand rest, a thumb groove, a set of finger grooves, passive soft stops, and/or any other additional elements. The aircraft control system can optionally include a flight controller, aircraft sensors, effectors, and a haptic feedback mechanism. However, the aircraft control system 100 can additionally or alternatively include any other suitable components.