Sensor-Guided Flight Mode Transition Control in Electric Aircraft
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Solution Overview
Problem
Modern electric aircraft lack an apparatus to guide smooth transitions between flight modes, making it difficult for pilots to control them effectively.
Innovation Solution
An apparatus comprising sensors to detect movement data and a flight controller that determines the current flight mode and generates guidance data to assist pilots in transitioning between modes, communicated through a pilot indicator.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Adaptability or versatility
If electric aircraft have multiple parts and systems to assist transition between flight modes, then the aircraft has more capabilities for mode transition, but the pilot control becomes more complex and difficult
Solution Approach 1:
The patent introduces a guidance system as an intermediary between the pilot and the aircraft's flight mode transition systems. This guidance system processes pilot inputs and coordinates the multiple parts and systems involved in mode transition, providing a simplified interface that reduces pilot workload while maintaining the aircraft's advanced transition capabilities
Solution Approach 2:
The patent implements a feedback mechanism where the guidance system continuously monitors the aircraft's flight mode and provides real-time guidance information to the pilot. This feedback loop helps the pilot understand the current flight mode and the transition status, making the control more intuitive despite the complexity of multiple underlying systems
2Ease of operation
If no guidance apparatus is provided for mode transition, then the aircraft system remains simple, but the pilot cannot effectively control smooth transitions between flight modes
Solution Approach 1:
The guidance system is designed to perform multiple functions: detecting movement data, determining current flight mode, generating guidance data, and communicating with the pilot. By consolidating these functions into a single multi-functional apparatus, the patent improves pilot control without proportionally increasing overall system complexity
3Productivity
If the aircraft lacks an apparatus to determine current flight mode and generate guidance data, then the system remains simple, but informed flight planning and power-saving flight plans cannot be achieved
Solution Approach 1:
The guidance system performs preliminary actions by continuously determining the current flight mode and generating guidance data before the pilot needs to make decisions. This advance preparation of flight information enables informed flight planning and power-saving strategies without requiring complex post-processing or additional systems
Data Source
AI summary
An apparatus for guiding a transition between flight modes of an electric aircraft is illustrated. The apparatus comprises at least a sensor configured to detect a movement datum of the electric aircraft and a flight controller communicatively connected to the at least sensor, wherein the flight controller is configured to receive the movement datum from the at least a sensor, determine a current flight mode of the electric aircraft as a function of a pilot input and the movement datum, generate a guidance datum as a function of a change in flight mode and the movement datum, and communicate the guidance datum to a pilot indicator in communication with the at least a sensor and flight controller communicatively connected to the at least a sensor.