UAV Altitude Control Using Terrain-Relative Flight Limits

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Solution Overview

Problem

Current altitude restrictions for UAVs are often inflexible and do not account for varying terrain or ground levels, leading to potential safety issues and compliance problems, as they are based on fixed reference levels like sea level without considering local elevations or complex terrains.

Innovation Solution

A system and method for dynamically adjusting altitude restrictions based on real-time elevation information and sensor data, allowing UAVs to modify their flight altitude relative to ground level, ensuring compliance with regulations and avoiding obstacles.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If fixed altitude restrictions based on sea level are used, then compliance with air traffic control regulations is simplified, but the UAV may encroach upon controlled airspace or fail to reach allowed heights in areas with varying terrain elevation

Engineering Contradiction:
Improvealtitude restriction adaptabilityVSAvoidaltitude control system complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The patent implements dynamic altitude restrictions that automatically adjust based on real-time GPS location and terrain elevation data. The system transitions from static fixed-altitude limits to dynamic terrain-relative limits, allowing the UAV to fly higher above ground level in high-altitude areas while maintaining compliance in low-altitude areas. This resolves the contradiction by making the altitude restriction system adaptable to varying terrain without requiring complex manual configuration.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system continuously monitors the UAV's GPS position, retrieves terrain elevation data from databases or sensors, and automatically adjusts the altitude restrictions accordingly. This closed-loop feedback mechanism ensures the UAV maintains proper clearance from controlled airspace while maximizing flight altitude above ground level, resolving the contradiction between adaptability and complexity through automated feedback-driven adjustment.

Inventive Principle:
Principle #23Feedback

2Reliability

If altitude restrictions are set relative to ground level, then the UAV can fly appropriate distances above terrain, but the system must continuously account for terrain elevation and altitude gradients

Engineering Contradiction:
Improveflight safetyVSAvoidelevation calculation complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent introduces an intermediary terrain elevation database or elevation sensor system that mediates between the UAV's position and the altitude restriction calculation. Rather than directly computing complex terrain relationships, the system uses this intermediary layer to provide ready-to-use elevation data, simplifying the reliability-critical calculations while maintaining safety through continuous terrain awareness.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Reliability

If remote controller fails, the UAV may continue flying upwards, but imposing strict altitude limits may restrict legitimate flight operations

Engineering Contradiction:
Improvefailure safetyVSAvoidflight operation flexibility
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The system pre-configures altitude restrictions and safety protocols before flight operations begin. By establishing terrain-relative altitude limits in advance and loading them into the UAV's flight controller, the system ensures that even if the remote controller fails, the UAV cannot exceed predetermined safe altitudes. This preliminary action protects against failure while maintaining operational flexibility within the established boundaries.

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS11687098B2Vehicle altitude restrictions and control
Publication Date: 2023.06.27 SZ DJI TECH CO LTD
  • US11687098B2 patent drawing
  • US11687098B2 patent drawing
  • US11687098B2 patent drawing

AI summary

An unmanned aerial vehicle (UAV) includes a vehicle body, one or more propulsion units coupled to the vehicle body and configured to effect movement of the UAV, and one or more processors coupled to the one or more propulsion units and individually or collectively configured to receive one or more sets of altitude restrictions for the UAV, receive location information indicating a current location of the UAV, determine a priority of the one or more sets of altitude restrictions by which the UAV abides based on the location information, select a set from the one or more sets of altitude restrictions based on the determined priority, and generate control signals to control the one or more propulsion units such that the UAV is operated in compliance with the selected set of altitude restrictions.