TY - JOUR
T1 - Path Planning to Improve Reachability in a Forced Landing
AU - Izuta, Shusuke
AU - Takahashi, Masaki
N1 - Publisher Copyright:
© 2016, Springer Science+Business Media Dordrecht.
PY - 2017/5/1
Y1 - 2017/5/1
N2 - 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.
AB - 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.
KW - Aircraft
KW - Forced landing
KW - Gliding
KW - Path planning
KW - Reachability Analysis
UR - http://www.scopus.com/inward/record.url?scp=84991781111&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=84991781111&partnerID=8YFLogxK
U2 - 10.1007/s10846-016-0431-3
DO - 10.1007/s10846-016-0431-3
M3 - Article
AN - SCOPUS:84991781111
SN - 0921-0296
VL - 86
SP - 291
EP - 307
JO - Journal of Intelligent and Robotic Systems: Theory and Applications
JF - Journal of Intelligent and Robotic Systems: Theory and Applications
IS - 2
ER -