Thursday, July 19, 2018

Automatic Take-off and Landing


Automatic Take-off and Landing

Simona Teodorovic

July, 2018
           
            A very simple search reveals various systems that have the capability of automatic take-off and landing. For decades, pilots of manned aircraft have been utilizing the autopilot, which later on has developed into the autoland. Debates and discussions are nowadays held, arguing what is the role of the pilot in the cockpit? How much, during the actual flight is he operating at the commands, as opposed to just overviewing them and managing input and output data? However, as far as technology in aviation has evolved, a completely automatic take-off of a manned aircraft has not yet been achieved (Can a Plane Land Automatically, n.d.).
            Any flight that is completely autonomous requires skillful precision in aircraft positioning. For landings and take-offs, this is of even greater importance (Wenzel, Masselli, & Zell, 2011). From the same source, we can see the authors developing a system that has the capability of automatic landing on a moving platform. Due to the size of the Unmanned Aerial Vehicle (UAV), the on-board space is very limited for implementing navigational aids and additional equipment.
            In contrast to the mentioned system, a fixed wing, blended wide body (BWB) has proven to be successful in automated phases of flight. This type aircraft has improved flight characteristics and advanced payload capabilities. Even though this vehicle cannot compete with those of the military, it demonstrates increased endurance, which for the purpose of this analysis allows for an illustration of its level of automation.
            According to Huh and Shim (2010), this type of aircraft can land automatically, by controlling this phase through “vision algorithms and relatively simple landing aids” (p. 218). This way, there would be no need for costly sensors and additional equipment. The overall system consists out of “an inflated dome as a visual marker, a vision processing unit, and a flight controller using a visual servoing algorithm” (p. 219). This technology offers a simply solution to automatic landing. Additionally, due to its simplicity, in the event of a malfunction, the system will be able to be transferred and operated by a pilot. Depending on the level of sophistication of the additional equipment, the aircraft has the ability to fly from an initial position to a final one, based on a partially recognized environment (Saripalli, Montgomery, & Sukhatme, 2002).       
            This type of system has many advantages. Low cost and maintenance, simplicity and GPS based navigation, allows for an easy transition between automated and manual flight. At this level of automation, a suggestion would be to further develop it. The structure of a BWB allows for greater payload, stability and an overall, positive performance.
            Many systems currently have the capability of automatic operations (Scan Eagle, Global Hawk, etc.). However, as much as it might reduce human factor issues, it arises new concerns. There are terrible consequences of landings that are not executed correctly and that fail. In other words, it would be preferable and beneficial if the operator could recognize and terminate a disastrous landing beforehand.





 References
Can a Plane Land Automatically. Retrieved on July 7th, 2018, from https://www.flightdeckfriend.com/can-a-plane-land-automatically
Huh, S., & Shim, D. H. (2010). A vision-based automatic landing method for fixed-wing UAVs. Journal of Intelligent and Robotic Systems, 57, 217-231. doi:10.1007/s10846-009-9382-2
Saripalli, S., Montgomery, J. F., & Sukhatme, G. S. (2002). Vision-based autonomous landing of an unmanned aerial vehicle. In Proceedings of IEEE International Conference on Robotics and Automation, 2779-2804. Washington, D.C., USA.
Wenzel, K. E., Masselli, A., & Zell, Andreas (2011). Automatic take-off, tracking and landing of a miniature UAV on a moving carrier vehicle. Journal of Intelligent and Robotic Systems, 61, 221-238. doi:10.1007/s10846-010-9473-0

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