Rotorcraft Propeller Sensing for Drift-Free Indoor Positioning
Find Innovative SolutionsGenerate Solutions
Solution Overview
Problem
Existing rotorcraft systems lack accurate and cost-effective navigational sensing, with current solutions being limited in accuracy, restricted to outdoor or indoor use, expensive, and power-intensive.
Innovation Solution
The system embeds simple sensors into the rotating propellers of a rotorcraft to provide low-cost sensing of bearing, elevation, and distance, enabling communication with base stations, other rotorcraft, and robots.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Measurement precision
If existing navigational sensing systems are used, then positioning capability is provided, but cost and power consumption increase significantly
Solution Approach 1:
The patent replaces complex mechanical/electronic navigation systems (GPS, inertial sensors, cameras) with a magnetic field-based sensing system. The rotor blades act as antennas that detect magnetic field signatures from transmission sources, substituting power-intensive mechanical and electronic systems with a simpler electromagnetic field interaction approach that consumes less power while providing positioning capability.
Solution Approach 2:
The system uses magnetic field signatures as a simplified copy or representation of position information, rather than directly using complex sensor data from multiple navigation systems. The magnetic field patterns serve as a lightweight informational copy that enables positioning without requiring the full complexity of traditional navigation stacks.
2Measurement precision
If existing navigational sensing systems are used, then positioning capability is provided, but system cost increases
Solution Approach 1:
The patent replaces expensive mechanical and electronic navigation systems with a magnetic field-based approach. Instead of using costly GPS receivers, inertial measurement units, and camera systems, the invention uses the rotor blades themselves as magnetic field sensors, dramatically reducing component costs while maintaining positioning functionality.
Solution Approach 2:
The rotor blades serve multiple functions: they generate lift/thrust for flight and simultaneously act as antennas for magnetic field detection. This multi-functionality eliminates the need for separate navigation hardware, reducing overall system cost while providing both propulsion and positioning capabilities.
3Adaptability or versatility
If existing navigational sensing systems are used, then outdoor navigation is enabled, but indoor navigation capability is lost
Solution Approach 1:
The patent replaces GPS-dependent navigation systems with magnetic field-based sensing that works independently of satellite signals. By using the Earth's magnetic field and local magnetic signatures from transmission sources, the system provides continuous navigation capability both outdoors and indoors, eliminating the outdoor/indoor limitation of GPS-based systems.
4Ease of manufacture
If simple sensor systems are used, then cost and power consumption are reduced, but measurement accuracy deteriorates
Solution Approach 1:
The system uses the dynamic rotation of rotor blades to sweep the magnetic field sensing capability in multiple directions. As the blades rotate, they detect magnetic field signatures from different angles and positions, dynamically gathering information that enhances positioning accuracy despite using simple sensor components. The motion itself becomes part of the sensing mechanism.
Solution Approach 2:
The rotating rotor blades perform periodic sensing sweeps of the magnetic field environment. Each rotation provides a complete 360-degree scan of magnetic signatures, and by analyzing the periodic pattern of detected fields over multiple rotations, the system can accurately determine position and orientation using simple sensors.
Data Source
AI summary
A system for determining positional information of a rotorcraft includes a central controller and a first sensor unit. The first sensor unit is mounted to a first rotating portion of the rotorcraft and is in communication with the central controller. The first sensor unit includes one or more first receivers configured to receive signals from a remote transmission source. The first sensor unit also includes a processor configured to determine a bearing of the rotorcraft relative to the remote transmission source based in part on the signals received from the remote transmission source. The first sensor unit further includes a transmitter configured to transmit the bearing of the rotorcraft to a central controller of the rotorcraft.


