Branch & Bound-Based Algorithm for Aircraft VNAV Profile Reference Trajectory Optimization

Author(s):  
Alejandro Murrieta Mendoza ◽  
Bruce Beuze ◽  
Laurane Ternisien ◽  
Ruxandra M. Botez
1999 ◽  
Vol 121 (4) ◽  
pp. 697-702
Author(s):  
C. C. H. Ma ◽  
T. W. T. Qian

An automatic trajectory optimization scheme, which takes the system dynamics into account, is presented in this paper. It is developed for use in conjunction with the rapid-tracking learning control. It optimizes the reference trajectory such that tracking will be speeded up whenever the actuator capability is not fully utilized, and slowed down whenever the actuator would otherwise saturate. This yields not only excellent fast tracking performance but also a new reference trajectory which accommodates the saturation constraint of the control actuator. Application of the proposed strategy in control practice will ease the burden of having to precisely design the timing of a reference trajectory in a tracking control problem. The resulting controlled system is able to precisely track short but highly complex trajectories at the highest speed physically possible. Simulation and experimental results of simultaneously controlling two motors to emulate servoing an x-y table are given to demonstrate the effectiveness of the proposed methodology.


Author(s):  
S. Yu. Chernikov ◽  
D. A. Blagodarov ◽  
Y. M. Safonov ◽  
L. O. Gosteva ◽  
N. N. Fedortsov

2008 ◽  
Vol 85 (4) ◽  
pp. 454-464 ◽  
Author(s):  
David K. Lam ◽  
Rhoda Baker ◽  
Christopher Le Swartz

2020 ◽  
Vol 314 ◽  
pp. 02002
Author(s):  
Alejandro Murrieta-Mendoza ◽  
Hugo Ruiz ◽  
Ruxandra Mihaela Botez

The increasing of flights around the world has led to various problems for the aeronautical industry such as saturated air space and higher levels of fossil fuel consumption. The way in which en-route flights are handled should be improved in order to increase airways’ capacity. A solution is to make aircraft to arrive at specific waypoints at a time constraint called Required Time of Arrival (RTA). Fossil fuel brings as a consequence the release of polluting particles to the atmosphere such as carbon dioxide and nitrogen oxides. It is thus desirable to compute the most economical trajectory in terms of fuel burn while fulfilling the RTA constraint. This article proposes a horizontal reference trajectory optimization algorithm based on the Particle Swarm Optimization technique in order to reduce fuel burn while fulfilling the RTA constraint. Results showed that for a flight without RTA constraint, up to 4% of fuel can be saved comparing against the trajectory of reference. The algorithm was normally able to meet the RTA constrain. However, aggressive RTA constraints might reduce the optimization levels of fuel compared with flights without RTA constraint.


Aerospace ◽  
2020 ◽  
Vol 7 (7) ◽  
pp. 99
Author(s):  
Alejandro Murrieta-Mendoza ◽  
Charles Romain ◽  
Ruxandra Mihaela Botez

Aircrafts require a large amount of fuel in order to generate enough power to perform a flight. That consumption causes the emission of polluting particles such as carbon dioxide, which is implicated in global warming. This paper proposes an algorithm which can provide the 3D reference trajectory that minimizes the flight costs and the fuel consumption. The proposed algorithm was conceived using the Floyd–Warshall methodology as a reference. Weather was taken into account by using forecasts provided by Weather Canada. The search space was modeled as a directional weighted graph. Fuel burn was computed using the Base of Aircraft DAta (BADA) model developed by Eurocontrol. The trajectories delivered by the developed algorithm were compared to long-haul flight plans computed by a European airliner and to as-flown trajectories obtained from Flightradar24®. The results reveal that up to 2000 kg of fuel can be reduced per flight, and flight time can be also reduced by up to 11 min.


2017 ◽  
Vol 30 (4) ◽  
pp. 1459-1472 ◽  
Author(s):  
Alejandro MURRIETA-MENDOZA ◽  
Bruce BEUZE ◽  
Laurane TERNISIEN ◽  
Ruxandra Mihaela BOTEZ

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