2010 IEEE Aerospace Conference 2010
DOI: 10.1109/aero.2010.5446773
|View full text |Cite
|
Sign up to set email alerts
|

A 3-phase safe trajectory shaping for a distressed aircraft

Abstract: A statistical flight plan optimization framework is developed, and a simplified version solved for a hypothetical distress situation. The framework proposed herein attempts to increase overall survivability by evaluating and optimizing the probable outcome of various flight plans, given a statistical representation of the probable outcomes of each flight plan and their respective probabilities of success. This work attempts to solve the problem using a simplified probability model and safety metric. An airport… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1
1

Citation Types

0
3
0

Year Published

2012
2012
2013
2013

Publication Types

Select...
3
1

Relationship

1
3

Authors

Journals

citations
Cited by 4 publications
(3 citation statements)
references
References 9 publications
(14 reference statements)
0
3
0
Order By: Relevance
“…The chosen landing site must be within this range for the sake of safety. It's different from the classical max range gliding problem and is also different from the flight plan optimization 2,15 . By the end of the descending maneuver, the aircraft must meet the final landing constraint (speed and attitude) to perform a safe touch down at landi ).…”
Section: Glide Trajectory Optimizationmentioning
confidence: 98%
“…The chosen landing site must be within this range for the sake of safety. It's different from the classical max range gliding problem and is also different from the flight plan optimization 2,15 . By the end of the descending maneuver, the aircraft must meet the final landing constraint (speed and attitude) to perform a safe touch down at landi ).…”
Section: Glide Trajectory Optimizationmentioning
confidence: 98%
“…With this information, the reachable landing site can be determined according to some flight planner [5], [6]. …”
Section: Estimation Of Gliding Rangementioning
confidence: 99%
“…There are four algorithms in DART-MSOP architecture as shown in Figure 2 and further details can be found in the references. [1][2][3][4][5][6][7][8][9][10][11][12][13][14] These four algorithms are: (a) low-fidelity initial turn algorithm; (b) high-fidelity paths with aborts; (c) guidance of a perpetual turning attitude aircraft to maneuvre to land safely, and (d) decision making. DART-MSOP is based on integration of four new algorithms developed that maximizes safe outcome probability after a distress event by incorporating an abort airport together with a model of current aircraft dynamics.…”
Section: Introductionmentioning
confidence: 99%