Automatic Takeoff Flight Control for Shorter Takeoff Distance

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Solution Overview

Problem

Current autopilot systems do not fully automate the takeoff process, leaving pilots to manually control aircraft during critical phases, which limits safety and efficiency.

Innovation Solution

The Enhanced Take-Off System (ETS) integrates with existing closed-loop fly-by-wire architecture to automate longitudinal and lateral control, using sensors and processors to optimize control surfaces deflection and reduce pilot workload, allowing the aircraft to follow predetermined control parameters from the moment it lifts off.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If manual control is used during takeoff, then pilot flexibility and adaptability are maintained, but pilot workload increases and safety decreases

Engineering Contradiction:
ImprovesafetyVSAvoidpilot workload
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The aircraft system performs takeoff control autonomously through the enhanced autopilot system, which automatically manages longitudinal and lateral control surfaces during takeoff without requiring continuous manual input from the pilot, thereby reducing workload while maintaining safety

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The system pre-configures optimal control parameters and trajectories before takeoff, allowing the autopilot to execute predetermined control sequences that ensure safety while minimizing the need for real-time pilot intervention

Inventive Principle:
Principle #10Preliminary action

2Reliability

If full automation is implemented during takeoff, then pilot workload is reduced and safety is improved, but system complexity increases

Engineering Contradiction:
ImprovesafetyVSAvoidsystem complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The enhanced takeoff system leverages the existing fly-by-wire architecture and autopilot components already present in modern aircraft, making the existing multi-functional system perform additional takeoff automation functions without requiring completely new dedicated hardware

Inventive Principle:
Principle #6Universality (Multi-functionality)

Solution Approach 2:

The system combines longitudinal and lateral control functions into a unified automated takeoff sequence, merging multiple control operations into a single integrated process that reduces overall system complexity while achieving full automation

Inventive Principle:
Principle #5Merging (Combining)

3Productivity

If manual control is used during takeoff, then system simplicity is maintained, but takeoff distance and weight increase

Engineering Contradiction:
Improvetakeoff efficiencyVSAvoidautomation level
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The enhanced autopilot system continuously monitors aircraft performance parameters during takeoff and automatically adjusts control surfaces based on real-time feedback, optimizing the takeoff trajectory to minimize distance and weight requirements while maintaining system simplicity through rule-based control logic

Inventive Principle:
Principle #23Feedback

Data Source

PatentUS11226639B2Enhanced take-off system
Publication Date: 2022.01.18 YABORA IND AERONAUTICA SA
  • US11226639B2 patent drawing
  • US11226639B2 patent drawing
  • US11226639B2 patent drawing

AI summary

An automatic takeoff flight control system controls an aircraft to automatically follow a predetermined set of control parameters upon taking off from the ground using both longitudinal and lateral control laws. The control system provides takeoff speed reduction to thereby reduce the takeoff distance (TOD) and, as a consequence, increase the takeoff weight (TOW). The control system sets the horizontal stabilizer (HSTAB) in a non-trimmed condition—named “mistrim”; and provides beta for optimum climb at takeoff, through lateral-directional surfaces commands.