Vehicle Stability Control for eLSD and Active Aero Actuators

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Solution Overview

Problem

Existing vehicle control systems face challenges in maintaining stability when using model predictive control (MPC) for electronic limited slip differentials and active aerodynamic actuators, as they may produce miscalculations due to inaccurate prediction models and conflict between control actions, leading to potential vehicle instability.

Innovation Solution

A system comprising a primary control module, a stability status module, and a supervisory control module that adjusts control actions in real-time to maintain vehicle stability by using a logic-based structure to manage integrated control systems, ensuring optimization constraints prevent instability and focus on main objectives.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If model predictive control is used for electronic limited slip differentials and active aerodynamic actuators, then vehicle control performance is improved, but miscalculations may occur due to inaccurate prediction models leading to vehicle instability

Engineering Contradiction:
Improvevehicle stabilityVSAvoidprediction model accuracy
Core Design Contradiction:
ReliabilityVSMeasurement precision

Solution Approach 1:

The system implements a supervisory control module that continuously monitors vehicle stability status and feeds this information back to adjust control actions. The stability status module assesses real-time stability conditions and provides feedback to the supervisory control module, which then modifies control inputs to prevent instability, creating a closed-loop feedback system that compensates for prediction model inaccuracies.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The supervisory control module acts as an intermediary between the primary model predictive control system and the actual actuators. It receives control actions from the primary controller, adjusts them based on real-time stability assessments, and then applies the modified control actions to the electronic limited slip differential and active aerodynamic actuators, preventing miscalculations from causing instability.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Adaptability or versatility

If multiple control actions are generated for integrated control systems, then control objectives are addressed, but conflict between control actions may occur leading to instability

Engineering Contradiction:
Improvecontrol objective coverageVSAvoidvehicle stability
Core Design Contradiction:
Adaptability or versatilityVSStability of the object's composition

Solution Approach 1:

The system merges multiple control actions from different control objectives into a single coordinated control strategy. The supervisory control module integrates control inputs for the electronic limited slip differential and active aerodynamic actuators, ensuring that control actions from different objectives work together harmoniously rather than conflicting, while maintaining vehicle stability.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The control system dynamically adjusts control actions based on real-time vehicle stability status. The supervisory control module continuously modifies control inputs according to current operating conditions, allowing the system to adapt to changing situations and resolve conflicts between control objectives dynamically rather than using fixed control strategies.

Inventive Principle:
Principle #15Dynamics

3Reliability

If control actions are adjusted in real-time to maintain stability, then vehicle stability is improved, but control system complexity increases

Engineering Contradiction:
Improvevehicle stabilityVSAvoidcontrol system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The control system is segmented into distinct functional modules: a primary control module for model predictive control, a stability status module for monitoring, and a supervisory control module for adjustment. This segmentation allows each module to perform its specific function independently, making the overall complex system more manageable and easier to implement while achieving real-time stability maintenance.

Inventive Principle:
Principle #1Segmentation

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

The system effectively maintains vehicle stability by adjusting control actions based on real-time stability assessments, reducing the risk of miscalculations and optimizing control inputs, especially for complex nonlinear systems, thereby enhancing vehicle performance and safety.

Implementation Method 1

The wing generates a downward force that is transmitted to the front or rear wheels of the vehicle. The attack angle of the wing is adjustable to adjust the amount of downward force generated by the wing.

Methodology Applied
Scientific EffectAerodynamic force: Aerofoil

Data Source

PatentUS11866032B2System and method for controlling electronic limited slip differential and active aerodynamic actuator on vehicle
Publication Date: 2024.01.09 GM GLOBAL TECHNOLOGY OPERATIONS LLC
  • US11866032B2 patent drawing
  • US11866032B2 patent drawing
  • US11866032B2 patent drawing

AI summary

A system includes a primary control module, a stability status module, and a supervisory control module. The primary control module is configured to determine at least one control action for at least one of an electronic limited slip differential and an aerodynamic actuator of a vehicle based on a driver command. The stability status module is configured to determine whether at least one component of the vehicle is stable or unstable based on an input from a sensor on the vehicle. The at least one component includes at least one of a vehicle body, a front axle, a rear axle, front wheels, and rear wheels. The supervisory control module is configured to adjust the at least one control action when the at least one component is unstable.