AUTOPILOT-BASED AIRCRAFT RECOVERY SYSTEM

Organization Name

Inventor(s)

Rostyslav Svitelskyi of Shoreline WA (US)

Brian Kenyon Rupnik of Lake Stevens WA (US)

AUTOPILOT-BASED AIRCRAFT RECOVERY SYSTEM - A simplified explanation of the abstract

This abstract first appeared for US patent application 20240262491 titled 'AUTOPILOT-BASED AIRCRAFT RECOVERY SYSTEM

Simplified Explanation: The patent application describes an aircraft with an autopilot system that can automatically control the flight of the aircraft using different control laws based on the operating condition.

Key Features and Innovation:

Autopilot system with one or more processors
Different control laws for different operating conditions
Automatic control of the aircraft's flight

Potential Applications: This technology can be applied in commercial aircraft, military drones, and unmanned aerial vehicles (UAVs) to enhance flight control and safety.

Problems Solved: This technology addresses the need for efficient and adaptive flight control systems that can respond to changing operating conditions during flight.

Benefits:

Improved flight control and safety
Enhanced efficiency in aircraft operations
Adaptability to different flight conditions

Commercial Applications: The technology can be utilized in the aviation industry for commercial airlines, defense applications, and drone operations, potentially leading to safer and more efficient flights.

Prior Art: Prior research in the field of autopilot systems and flight control algorithms can provide valuable insights into the development and implementation of this technology.

Frequently Updated Research: Stay updated on advancements in aviation technology, autopilot systems, and flight control algorithms to understand the latest trends and innovations in the field.

Questions about Aircraft Autopilot Systems: 1. How do different control laws impact the performance of an aircraft's autopilot system? 2. What are the key considerations when designing adaptive flight control algorithms for varying operating conditions?

Original Abstract Submitted

an aircraft includes an autopilot system including one or more processors. the one or more processors are configured to, in response to selection of an autopilot activation button during flight of the aircraft while the aircraft is operating in a first condition, apply first control laws to automatically control the flight of the aircraft. the one or more processors are further configured to, in response to selection of the autopilot activation button while the aircraft is operating in a second condition, apply second control laws to automatically control the flight of the aircraft, where the second control laws are different from the first control laws.