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| en:safeav:hw:sensingtechnologies [2026/06/17 12:16] – tgrzejszczak | en:safeav:hw:sensingtechnologies [2026/06/17 13:13] (current) – [Domain Constraints and Emerging Frontiers] tgrzejszczak |
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| Unmanned Aerial Vehicles (UAVs) operate in safety-critical, three-dimensional spaces where hardware design is strictly governed by payload weight and power constraints. Sensing in the airborne domain prioritizes high-fidelity attitude and altitude estimation, utilizing barometers and Inertial Measurement Units (IMUs) that must be verified for bounded, deterministic execution. Unlike ground systems, airborne autonomy requires sensing that remains reliable in "loss-of-link" scenarios and must support strict envelope protection across all flight phases. | Unmanned Aerial Vehicles (UAVs) operate in safety-critical, three-dimensional spaces where hardware design is strictly governed by payload weight and power constraints. Sensing in the airborne domain prioritizes high-fidelity attitude and altitude estimation, utilizing barometers and Inertial Measurement Units (IMUs) that must be verified for bounded, deterministic execution. Unlike ground systems, airborne autonomy requires sensing that remains reliable in "loss-of-link" scenarios and must support strict envelope protection across all flight phases. |
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| | <figure Ref.Pic.1> |
| | {{:en:safeav:hw:environmental_stressors.png?nolink&400 | environmental_stressors}} |
| | <caption>Comparative technical analysis of environmental stressor</caption> |
| | </figure> |
| Figure: Comparative technical analysis of environmental stressors, highlighting radiation in space, corrosion in marine, weight in air, and obstacle density on ground. This figure is draft/placeholder. | Figure: Comparative technical analysis of environmental stressors, highlighting radiation in space, corrosion in marine, weight in air, and obstacle density on ground. This figure is draft/placeholder. |
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