Autonomous Light Aircraft Control for Pilotless Payload Flight

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Solution Overview

Problem

Current autonomous vehicles, such as drones and light aircraft, face safety concerns and weight limitations that hinder their utility for tasks like cargo transfer and human transport, and require a certified pilot, limiting their mainstream viability and range.

Innovation Solution

An autonomous light aircraft system that operates without an onboard pilot, utilizing a temporal vector integration engine for precise navigation, integrates with traffic and air traffic control systems, and includes safety features for human transport, enabling autonomous flight and landing at designated sites or intersections, with the ability to adapt to changing regulations and obstacles.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Quantity of substance

If the vehicle weight exceeds 212 pounds to achieve higher lift capability and payload capacity, then the vehicle can transport more cargo and passengers, but the vehicle is reclassified from UAV to Sport Light Aircraft requiring a certified pilot

Engineering Contradiction:
Improvepayload capacityVSAvoidpilot requirement
Core Design Contradiction:
Quantity of substanceVSEase of operation

Solution Approach 1:

The aircraft is equipped with an autonomous flight management system that performs navigation, obstacle detection, and flight control functions independently without requiring a human pilot. The system integrates sensors, processors, and control actuators to enable the aircraft to service itself during flight operations, thereby eliminating the pilot requirement while maintaining regulatory compliance for aircraft over 212 pounds.

Inventive Principle:
Principle #25Self-service

2Extent of automation

If traditional drone control systems are used, then the vehicle can operate autonomously, but safety concerns and weight limitations restrict utility for human transport and cargo transfer

Engineering Contradiction:
Improveautonomous operationVSAvoidsafety
Core Design Contradiction:
Extent of automationVSReliability

Solution Approach 1:

The autonomous flight system is divided into separate functional modules including obstacle detection subsystem, navigation subsystem, control subsystem, and communication subsystem. Each module independently performs its specific function with dedicated sensors and processors, allowing for modular safety verification and reducing system-wide failure risks while maintaining high autonomous operation capability.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system incorporates redundant safety systems and fail-safe mechanisms that are pre-configured to activate automatically upon detecting system failures or unsafe conditions. Multiple independent sensors and control pathways provide backup capabilities, ensuring continued safe operation or controlled landing even when primary systems malfunction, thereby addressing safety concerns before they manifest as failures.

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

3Ease of operation

If autonomous navigation systems are integrated to enable pilotless flight, then the vehicle can operate without a certified pilot, but complexity of control systems increases

Engineering Contradiction:
Improvepilotless flight capabilityVSAvoidcontrol system complexity
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The flight control system is designed with universal modules that can adapt to different flight modes and operational requirements. The same hardware platform supports both autonomous operation and potential manual override capabilities, and the software architecture allows configuration for various mission profiles. This multi-functionality reduces overall system complexity by eliminating the need for separate dedicated systems for different operational modes.

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

Data Source

PatentUS12448122B2System and method for autonomous light aircraft operation
Publication Date: 2025.10.21 BIRKET IP HLDG INC
  • US12448122B2 patent drawing
  • US12448122B2 patent drawing
  • US12448122B2 patent drawing

AI summary

Unmanned Aerial Vehicles also known as UAVs or Drones, either autonomous or remotely piloted, are classified as drones by the US Federal Aviation Administration (FAA) as weighing under 212 pounds. The system described herein details Autonomous Flight Vehicles (AFV) which weigh over 212 pounds but less than 1,320 pounds which may require either a new classification or a classification such as Sport Light Aircraft, but without the requirement of a pilot due to the safe autonomous flight system such as the Safe Temporal Vector Integration Engine or STeVIE. Safe Autonomous Light Aircraft (SALA) are useful as drone carriers, large scale air package or cargo transport, and even human transport depending on the total lift capability of the platform.