Vehicle-Mounted Aircraft Landing Control for Fixed Camera Orientation

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Solution Overview

Problem

Existing aircraft systems that attach to vehicles for photography face challenges in maintaining a consistent photographing direction after landing, leading to instability and reduced usability of captured images.

Innovation Solution

An on-vehicle aircraft control system that includes a winding device on the landing platform, a connecting member, and a controller to control the aircraft's attitude, ensuring the photographing unit faces a specified direction upon landing by winding up the connecting member and adjusting the aircraft's attitude.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If the aircraft is used for photographing after landing on the vehicle, then the aircraft can be used for a wider range of purposes and can be more convenient, but the photographing direction varies depending on the attitude of the aircraft when landing, making it difficult to effectively use the photographed image

Engineering Contradiction:
Improveusability of aircraftVSAvoidphotographing direction stability
Core Design Contradiction:
Adaptability or versatilityVSReliability

Solution Approach 1:

The control device determines a specified photographing direction in advance before the aircraft lands. This preliminary determination of the desired photographing direction allows the system to prepare the appropriate attitude instructions beforehand, ensuring that the aircraft will be in the correct orientation for stable photographing immediately upon landing, thus preventing direction variation while maintaining versatility

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The control device receives attitude information from the aircraft and compares it with the predetermined specified photographing direction. Based on this feedback, the control device generates appropriate attitude instructions to guide the aircraft toward the correct orientation. This closed-loop feedback mechanism ensures the photographing direction remains stable and consistent with the predetermined specification

Inventive Principle:
Principle #23Feedback

Data Source

PatentUS11807363B2On-vehicle aircraft control system
Publication Date: 2023.11.07 MAZDA MOTOR CORP
  • US11807363B2 patent drawing
  • US11807363B2 patent drawing
  • US11807363B2 patent drawing

AI summary

An on-vehicle aircraft control system includes a winding device provided on a landing platform, a connecting member connecting the winding device and an aircraft and wound up or drawn out by the winding device, and a controller controlling the winding device and the aircraft. Upon receipt of a landing request to land the aircraft on the landing platform, the controller winds up the connecting member by the winding device and controls an attitude of the aircraft so as to land the aircraft with a photographing unit provided on the aircraft facing in a specified photographing direction determined in advance.