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Aerial Refueling Hose-Drogue Simulation Program



Product: Aerial Refueling Hose-Drogue Simulation Program

Development Stage: Pre-Market Validation

Primary Inventors: Kapseong Ro PhD, Assoc. Professor, Mechanical/Aeronautical Engineering Dept.

Scientific Publication: Ro et al., AIAA Guidance, Navigation, and Control Conference. 2010 - 8400

License Status: Available for licensing

IP Status: Copyright

Reference: 2011-010

Contact: Clark Bennett PhD
dclark.bennett@wmich.edu
269-387-8218

Download PDF



     Presently, two aerial refueling methods are practiced. One method uses a hose-drogue-probe assembly for the delivery of fuel. Probe-drogue refueling (PDR) involves coupling a probe on a receiver aircraft with a probe receptacle (drogue) attached to a flexible, fuel hose from the tanker aircraft.  PDR requires skillful piloting to maneuver the 4 inch probe into the center of a two foot diameter moving drogue, while flying at a relatively high rate of speed. At the moment of probe contact with the drogue, the drag force on the drogue decreases due to loss of tension, resulting in erratic motion of the refueling hose. Unless carefully regulated, this may lead to critical damage to the refueling assembly and the receiver probe.
     PDR has always been a technically challenging operation that often results in mishaps and damage. Therefore, there has been interest in an active control system on the drogue to limit drogue motion and to steer it to a predetermined position relative to the tanker. Also, improvements to receiver probe design are sought that can eliminate stress overloads in the probe and the hose-drogue system during the coupling and refueling phase. In addition, automated aerial refueling procedures have been under development in recent years and will be of great utility for refueling of unmanned aerial vehicles (UAV). Required for development of any new system for PDR is accurate simulation of the effect of turbulence on drogue and hose motion.

Technology Description
     Dr. Kapseong Ro has developed a dynamic software model that accurately captures the motion of a hose-drogue assembly affected by the prescribed motion of a tanker and receiver aircraft. The model is incorporated in a MATLAB/SIMULINK® software program that simulates the movements of hose-drogue refueling systems during aircraft refueling maneuvers.  The program predicts the hose-drogue motion in 3-D space (trajectory) versus time in response to tanker motion and wake generation, atmospheric turbulence, and approaching receiver aircraft fore-body aerodynamic effect. The program also predicts the post-contact wave motion of the hose for different closure-rates of the receiver aircraft and tension changes in the hose.
     This program has been utilized to design a drogue active control system, and is useful for designing more robust drogue and probe hardware, developing automated aerial refueling systems, in addition to novel actively controlled drogues.

Potential Benefits
  • Permits testing of designs for improvements to PDR before and during development
  • Utilizes MATLAB/SIMULINK® software structure, interface
  • Simulates effects of tanker and aircraft turbulence, and atmospheric turbulence on hose drogue assembly
  • Predicts wave motion of refueling hose due to loss of tension after coupling for different closure-rates

Aerial Refueling Hose-Drogue Simulation Program


     Presently, two aerial refueling methods are practiced. One method uses a hose-drogue-probe assembly for the delivery of fuel. Probe-drogue refueling (PDR) involves coupling a probe on a receiver aircraft with a probe receptacle (drogue) attached to a flexible, fuel hose from the tanker aircraft.  PDR requires skillful piloting to maneuver the 4 inch probe into the center of a two foot diameter moving drogue, while flying at a relatively high rate of speed. At the moment of probe contact with the drogue, the drag force on the drogue decreases due to loss of tension, resulting in erratic motion of the refueling hose. Unless carefully regulated, this may lead to critical damage to the refueling assembly and the receiver probe.
     PDR has always been a technically challenging operation that often results in mishaps and damage. Therefore, there has been interest in an active control system on the drogue to limit drogue motion and to steer it to a predetermined position relative to the tanker. Also, improvements to receiver probe design are sought that can eliminate stress overloads in the probe and the hose-drogue system during the coupling and refueling phase. In addition, automated aerial refueling procedures have been under development in recent years and will be of great utility for refueling of unmanned aerial vehicles (UAV). Required for development of any new system for PDR is accurate simulation of the effect of turbulence on drogue and hose motion.

Technology Description
     Dr. Kapseong Ro has developed a dynamic software model that accurately captures the motion of a hose-drogue assembly affected by the prescribed motion of a tanker and receiver aircraft. The model is incorporated in a MATLAB/SIMULINK® software program that simulates the movements of hose-drogue refueling systems during aircraft refueling maneuvers.  The program predicts the hose-drogue motion in 3-D space (trajectory) versus time in response to tanker motion and wake generation, atmospheric turbulence, and approaching receiver aircraft fore-body aerodynamic effect. The program also predicts the post-contact wave motion of the hose for different closure-rates of the receiver aircraft and tension changes in the hose.
     This program has been utilized to design a drogue active control system, and is useful for designing more robust drogue and probe hardware, developing automated aerial refueling systems, in addition to novel actively controlled drogues.

Potential Benefits
  • Permits testing of designs for improvements to PDR before and during development
  • Utilizes MATLAB/SIMULINK® software structure, interface
  • Simulates effects of tanker and aircraft turbulence, and atmospheric turbulence on hose drogue assembly
  • Predicts wave motion of refueling hose due to loss of tension after coupling for different closure-rates

Product: Aerial Refueling Hose-Drogue Simulation Program

Development Stage: Pre-Market Validation

Primary Inventors: Kapseong Ro PhD, Assoc. Professor, Mechanical/Aeronautical Engineering Dept.

Scientific Publication: Ro et al., AIAA Guidance, Navigation, and Control Conference. 2010 - 8400

License Status: Available for licensing

IP Status: Copyright

Reference: 2011-010

Contact: Clark Bennett PhD
dclark.bennett@wmich.edu
269-387-8218

Download PDF