scholarly journals Military aircraft mission planning: a generalized vehicle routing model with synchronization and precedence

2013 ◽  
Vol 2 (1-2) ◽  
pp. 109-127 ◽  
Author(s):  
Nils-Hassan Quttineh ◽  
Torbjörn Larsson ◽  
Kristian Lundberg ◽  
Kaj Holmberg
Keyword(s):  
Vehicle Routing ◽  
Mission Planning ◽  
Military Aircraft

A Time-Indexed Generalized Vehicle Routing Model for Military Aircraft Mission Planning

2016 ◽  
pp. 605-611
Author(s):  
Jorne Van den Bergh ◽  
Nils-Hassan Quttineh ◽  
Torbjörn Larsson ◽  
Jeroen Beliën
Keyword(s):  
Vehicle Routing ◽  
Mission Planning ◽  
Military Aircraft

scholarly journals Military aircraft mission planning

2014 ◽  
Vol 9 (8) ◽  
pp. 1625-1639 ◽  
Author(s):  
Nils-Hassan Quttineh ◽  
Torbjörn Larsson
Keyword(s):  
Mission Planning ◽  
Military Aircraft

Achievements of Military Aircraft

1913 ◽  
Vol 108 (14) ◽  
pp. 306-307
Author(s):  
H. Bannerman-Phillips
Keyword(s):  
Military Aircraft

Design and mission planning of Bobcat-1, the Ohio University CubeSat

2020 ◽  
Author(s):  
Kevin Croissant ◽  
Gregory Jenkins ◽  
Ryan McKnight ◽  
Brian C. Peters ◽  
Sabrina Ugazio ◽  
...  
Keyword(s):  
Mission Planning ◽  
Ohio University

A Method to Describe the Process of Shaping Operational Effectiveness of Military Aircraft – An Outline

2013 ◽  
Vol 33 (1) ◽  
pp. 45-55
Author(s):  
Henryk Tomaszek ◽  
Ryszard Kaleta ◽  
Mariusz Zieja
Keyword(s):  
Support Function ◽  
Military Aircraft ◽  
Operational Effectiveness ◽  
Correct Operation ◽  
Operation And Maintenance

Abstract The paper deals with the process of shaping the operational effectiveness of military aircraft under some specific circumstances, i.e. while flying on missions. The term ‘effectiveness’ has been assumed to mean the probability of accomplishing an air mission by one of the aeronautical system’s components, i.e. the aircraft together with its pilot. There is a chance to improve the effectiveness, or make it worse, in subsequent flights, depending on how the maintenance support function. The correct operation and maintenance of the system’s components should provide that the following condition is satisfied: * Pk ≥ P , where Pk - effectiveness in the k-th flight, and P* - the lower demanded limit of effectiveness. The Authors drew their inspiration for this paper from publication [2].

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