Path Planning to Improve Reachability in a Forced Landing
Autor: | Masaki Takahashi, Shusuke Izuta |
---|---|
Rok vydání: | 2016 |
Předmět: |
020301 aerospace & aeronautics
0209 industrial biotechnology Engineering business.industry Mechanical Engineering Measure (physics) ComputerApplications_COMPUTERSINOTHERSYSTEMS Thrust 02 engineering and technology Tracking (particle physics) Industrial and Manufacturing Engineering Precision approach radar 020901 industrial engineering & automation 0203 mechanical engineering Artificial Intelligence Control and Systems Engineering Reachability SAFER Motion planning Electrical and Electronic Engineering Descent (aeronautics) business Software Simulation |
Zdroj: | Journal of Intelligent & Robotic Systems. 86:291-307 |
ISSN: | 1573-0409 0921-0296 |
DOI: | 10.1007/s10846-016-0431-3 |
Popis: | This paper proposes a novel path planning method for improving the feasibility of a forced landing. When an aircraft completely loses its thrust, the only measure it can take is to make a forced landing at an adjacent airport as soon as possible. In such a situation, the flight path to the landing point must be safe and viable. This paper details a method which enables safer and easier landing by transferring the benefits of excess altitude to the final approach length. Moreover, by planning the descent angle of final approach to be in the middle of a non-spoiler and a full-spoiler glide angle, this method enables a change in descent angle to correct any tracking errors, without using thrust. To verify the effectiveness of the proposed method, six degrees-of-freedom nonlinear simulations were performed and the results are compared with comparable methods. From the simulation results, it was confirmed that the proposed method could plan a safe path in a sufficiently short time and the aircraft could reach the landing point safely. |
Databáze: | OpenAIRE |
Externí odkaz: |