RPA Flight Control Link Selection Based on Operation Risk

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Solution Overview

Problem

Existing flight control systems for Remotely Piloted Aircraft (RPA) require low-latency, proprietary, and often military-grade communication links that are expensive and not suitable for commercial use due to restricted radio frequency bands and high RF power levels, limiting their applicability.

Innovation Solution

A flight control system that includes an RPA and a ground-based control centre configured to communicate using multiple communication systems, allowing selection of a more reliable or lower-cost system based on operation risk, utilizing WiFi, cellular, and satellite communication systems, and incorporating risk assessment algorithms to manage operations safely and efficiently.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If proprietary military-grade communication links are used, then reliability is improved, but cost increases and commercial applicability decreases

Engineering Contradiction:
Improvecommunication reliabilityVSAvoidcommercial applicability
Core Design Contradiction:
ReliabilityVSAdaptability or versatility

Solution Approach 1:

The system dynamically selects communication systems based on operational risk assessment. The computer system evaluates risk factors and automatically chooses between different communication systems (satellite, cellular, WiFi, radio) to maintain reliable control while adapting to commercial operational contexts and cost constraints.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The flight control system is designed to work with multiple types of communication systems simultaneously. It can operate with satellite communication for high-reliability missions, cellular networks for moderate-risk operations, and WiFi or radio for low-risk commercial applications, making the system universally applicable across different commercial use cases.

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

2Speed

If low-latency communication links are used, then control responsiveness is improved, but cost increases

Engineering Contradiction:
Improvecontrol responsivenessVSAvoidcost-effectiveness
Core Design Contradiction:
SpeedVSAdaptability or versatility

Solution Approach 1:

The system dynamically adjusts communication requirements based on operational phase and risk assessment. During critical phases like takeoff and landing, it uses low-latency satellite or cellular links. During stable cruise phases with lower risk, it can switch to higher-latency but lower-cost communication systems, optimizing both responsiveness and cost-effectiveness.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system changes communication parameters such as data transmission frequency and latency tolerance based on operational context. For low-risk commercial operations, it increases latency tolerance to enable use of cheaper communication infrastructure, while maintaining safety through risk-based adaptive control strategies.

Inventive Principle:
Principle #35Parameter changes

3Reliability

If restricted RF licensed bands and high RF power levels are used, then communication reliability is improved, but legislative compliance becomes difficult and cost increases

Engineering Contradiction:
Improvecommunication reliabilityVSAvoidlegislative compliance
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The system is designed to operate across multiple radio frequency bands and communication standards. It can switch between licensed and unlicensed bands, and between different power levels, depending on legislative requirements of the operating region. This multi-functionality enables compliance with diverse international regulations while maintaining reliable communication.

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

Solution Approach 2:

The system dynamically adjusts RF power levels and frequency band selection based on operational context and legislative constraints. For commercial operations in regulated environments, it operates at lower power levels in licensed bands. For remote operations where legislation allows, it can increase power levels to maintain reliability, thus adapting to different regulatory frameworks.

Inventive Principle:
Principle #35Parameter changes

Data Source

PatentUS20260080784A1Flight control systems, ground-based control centres, remotely piloted aircraft, and method
Publication Date: 2026.03.19 FLYLOGIX HLDG LTD
  • US20260080784A1 patent drawing
  • US20260080784A1 patent drawing
  • US20260080784A1 patent drawing

AI summary

There is disclosed a flight control system, the flight control system including a Remotely Piloted Aircraft (RPA) and a ground-based control centre, wherein the RPA and the ground-based control centre are configured to communicate using a plurality of different communication systems, wherein the RPA includes a computer system configured to determine operation risk, wherein the computer system receives input from the ground-based control centre for use in the determination of operation risk, wherein the computer system is configured to select a communication system from the plurality of different communication systems, and to use the selected communication system for communication between the RPA and the ground-based control centre, based on the determined operation risk.