Single-Inceptor Aircraft Control With Haptic Self-Centering

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Solution Overview

Problem

Existing aircraft control systems require multiple input mechanisms and complex human controls, leading to high cognitive workload and reduced efficiency in managing feedback systems, especially in complex flight environments.

Innovation Solution

A unified aircraft control system utilizing a single inceptor that integrates a hand rest and passive soft stops, enabling reduced input mechanisms and self-centering to a neutral position, with haptic feedback to minimize cognitive load and streamline control inputs.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If multiple input mechanisms are used in existing aircraft control systems, then control functionality is comprehensive, but cognitive workload increases and efficiency decreases

Engineering Contradiction:
Improvecontrol functionalityVSAvoidnumber of input mechanisms
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The patent merges multiple input mechanisms into a single control stick that integrates multiple control functions. The control stick includes a grip portion, trigger portion, and throttle portion that can be manipulated with one hand to provide comprehensive control functionality while reducing the number of separate input devices the pilot must manage.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The control stick is designed as a universal control device that performs multiple functions through different manipulation methods. The same control stick can provide pitch control, roll control, throttle control, and other flight parameters through various input mechanisms integrated into a single device, allowing one component to replace multiple specialized controls.

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

2Measurement precision

If multiple feedback systems are implemented, then control precision is improved, but system complexity and mass increase

Engineering Contradiction:
Improvecontrol precisionVSAvoidnumber of feedback systems
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent combines multiple feedback mechanisms into an integrated control system where force feedback, position feedback, and haptic feedback are merged into the single control stick structure. This integration provides precise control information to the pilot through unified feedback channels rather than separate feedback systems.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The control stick incorporates force feedback mechanisms that provide tactile information to the pilot about aircraft state and control inputs. This feedback system allows the pilot to sense aircraft parameters and control forces directly through the control stick, improving control precision without requiring complex visual or electronic feedback displays.

Inventive Principle:
Principle #23Feedback

3Reliability

If complex human controls are used, then control authority is maintained, but ease of operation decreases

Engineering Contradiction:
Improvecontrol authorityVSAvoidcognitive workload
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The control stick incorporates self-centering mechanisms and force feedback systems that automatically guide the control input back to neutral positions and provide tactile cues for proper control application. This self-service functionality reduces the cognitive burden on the pilot by providing automatic guidance and feedback, allowing maintainment of control authority with reduced mental effort.

Inventive Principle:
Principle #25Self-service

Data Source

PatentUS12576962B2Aircraft control system and method
Publication Date: 2026.03.17 JOBY AERO INC
  • US12576962B2 patent drawing
  • US12576962B2 patent drawing
  • US12576962B2 patent drawing

AI summary

The aircraft control system 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 can additionally or alternatively include any other suitable components.