Honeywell international inc. (20240265815). SYSTEMS AND METHODS FOR GENERATING A MODIFIED FLIGHT PATH TO AVOID A NO TURN SITUATION simplified abstract
Contents
- 1 SYSTEMS AND METHODS FOR GENERATING A MODIFIED FLIGHT PATH TO AVOID A NO TURN SITUATION
- 1.1 Organization Name
- 1.2 Inventor(s)
- 1.3 SYSTEMS AND METHODS FOR GENERATING A MODIFIED FLIGHT PATH TO AVOID A NO TURN SITUATION - A simplified explanation of the abstract
- 1.4 Simplified Explanation
- 1.5 Key Features and Innovation
- 1.6 Potential Applications
- 1.7 Problems Solved
- 1.8 Benefits
- 1.9 Commercial Applications
- 1.10 Questions about the Technology
- 1.11 Original Abstract Submitted
SYSTEMS AND METHODS FOR GENERATING A MODIFIED FLIGHT PATH TO AVOID A NO TURN SITUATION
Organization Name
Inventor(s)
Suresh Bazawada of Phoenix AZ (US)
Anil Kumar Songa of Bangalore (IN)
Bojanapu Naresh of Hyderabad (IN)
SYSTEMS AND METHODS FOR GENERATING A MODIFIED FLIGHT PATH TO AVOID A NO TURN SITUATION - A simplified explanation of the abstract
This abstract first appeared for US patent application 20240265815 titled 'SYSTEMS AND METHODS FOR GENERATING A MODIFIED FLIGHT PATH TO AVOID A NO TURN SITUATION
Simplified Explanation
The patent application describes a system and method for adjusting a flight path to avoid obstacles. It involves receiving the current flight path and aircraft location data, retrieving terrain data, determining if the flight path leads to a no-turn situation, and displaying notifications for a modified flight path if necessary.
- The system receives the current flight path and aircraft location data.
- Terrain data is retrieved from an onboard database.
- It determines if the current flight path leads to a no-turn situation with respect to terrain obstacles.
- Notifications are displayed for implementing a modified flight path if needed.
Key Features and Innovation
- Integration of current flight path, aircraft location data, and terrain data to assess potential obstacles.
- Real-time notifications for pilots to adjust flight paths to avoid no-turn situations.
- Utilization of onboard sensors and databases to enhance flight safety.
Potential Applications
This technology can be applied in aviation for enhancing flight safety and avoiding potential obstacles during flights. It can also be utilized in unmanned aerial vehicles (UAVs) for autonomous obstacle avoidance.
Problems Solved
- Prevents aircraft from entering no-turn situations that could lead to collisions or accidents.
- Enhances pilot awareness of terrain obstacles in real-time.
- Improves overall flight safety and efficiency.
Benefits
- Increased safety for aircraft and passengers.
- Real-time decision-making support for pilots.
- Enhanced situational awareness during flights.
Commercial Applications
- Commercial airlines can use this technology to improve flight safety and efficiency.
- UAV manufacturers can integrate this system for autonomous obstacle avoidance in their products.
- Aviation authorities can implement this technology to enhance air traffic management systems.
Questions about the Technology
How does this technology improve flight safety?
This technology improves flight safety by providing real-time notifications to pilots about potential obstacles, allowing them to adjust flight paths accordingly.
What are the potential applications of this technology beyond aviation?
This technology can also be applied in other industries that require obstacle avoidance systems, such as autonomous vehicles and maritime navigation.
Original Abstract Submitted
systems and methods are provided for generating a modified flight to avoid a no turn situation. a current flight path of an aircraft is received from a source of current flight path of the aircraft. current aircraft location data is received from at least one geospatial sensor of the aircraft. terrain data is retrieved from an onboard database based on the current aircraft location data. the terrain data includes a first terrain obstacle and a second terrain obstacle. a determination is made regarding whether the current flight path of the aircraft leads to a no turn situation with respect to the first terrain obstacle and the second terrain obstacle. a first notification associated with implementation of a modified flight path in accordance with a viable turn with respect to the first terrain obstacle and the second terrain obstacle is displayed on an onboard display device based on the determination.
