Stereoscopic UAV Flight Simulator with Performance Monitoring

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Solution Overview

Problem

The challenge is to accurately test the effects of new equipment on unmanned aerial vehicles (UAVs) without actual flight, as existing methods face difficulties in isolating the exact impact on processor power, memory, and communication systems due to software and hardware interdependencies, and the risk of crashes from overloading with new sensors like stereoscopic cameras.

Innovation Solution

A controlled simulation environment using multiple video screens to provide accurate stereoscopic rendering, allowing UAVs to simulate flight scenarios while tethered, with a test computer monitoring system performance and providing navigation data to isolate the effects of new sensors on processor, memory, and communication systems.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If new equipment such as stereoscopic cameras is added to UAVs, then functionality and sensing capability are improved, but system complexity and risk of crashes increase due to processor overload and software incompatibilities

Engineering Contradiction:
Improvesensing capabilityVSAvoidcrash risk
Core Design Contradiction:
Adaptability or versatilityVSReliability

Solution Approach 1:

The patent applies preliminary action by conducting simulation tests before actual deployment. The system pre-tests new equipment configurations in a virtual environment to identify potential crashes and software incompatibilities before they occur in real UAV operations, thereby preventing crashes rather than responding to them after occurrence.

Inventive Principle:
Principle #10Preliminary action

2Measurement precision

If actual flight testing with new sensors is conducted, then real-world performance data is obtained, but costs and risks increase due to fuel consumption, weather dependencies, and potential damage

Engineering Contradiction:
Improveperformance data accuracyVSAvoidtesting cost
Core Design Contradiction:
Measurement precisionVSLoss of energy

Solution Approach 1:

The patent applies copying by creating a virtual copy of the real-world environment through simulation. Instead of conducting physical flight tests that consume fuel and incur costs, the system uses a digital replica of flight conditions to gather performance data, eliminating energy loss while maintaining measurement precision through accurate virtual modeling.

Inventive Principle:
Principle #26Copying

3Loss of energy

If controlled simulation testing is used instead of actual flight, then costs and risks are reduced, but difficulty in isolating exact impact on system components increases due to software and hardware interdependencies

Engineering Contradiction:
Improvetesting costVSAvoidcomponent impact isolation
Core Design Contradiction:
Loss of energyVSDifficulty of detecting and measuring

Solution Approach 1:

The patent applies segmentation by breaking down the integrated software-hardware system into separable components for independent testing. The simulation environment allows individual system components to be tested in isolation by selectively enabling or disabling specific sensors and processing chains, making it possible to measure the exact impact of each component despite the overall system interdependencies.

Inventive Principle:
Principle #1Segmentation

Data Source

PatentUS10703508B1Stereoscopic flight simulator with data acquisition
Publication Date: 2020.07.07 AMAZON TECH INC
  • US10703508B1 patent drawing
  • US10703508B1 patent drawing
  • US10703508B1 patent drawing

AI summary

Systems, apparatuses, and methods provide simulations to vehicles, such as unmanned aerial vehicles (UAVs) equipped with stereoscopic cameras. The system can include a plurality of screens set at predetermined angles to provide proper parallax to the stereoscopic cameras. The system can also include a test computer to update the screens based on the actions and travel time of the UAV. The test computer can also monitor the load on the computing systems of the UAV due to the camera and other inputs. The system can enable the testing and configuration of cameras and sensors without requiring actual flight. The test computer can provide navigational information to the UAV, receive actions taken by the UAV, update the screens based on these actions and the travel speed and direction of the UAV, and monitor the effects of the cameras and other sensors on the internal components of the UAV during use.