Aircraft performance in slippery runway conditions : a simulation study of the accuracy and limitations of real-time runway friction estimation based on airplane onboard data.

Details

• Creators:
  van Es, Gerard W.H. ; van der Geest, Peter J. ; Cheng, Andrew ; Stimson, Don
• Corporate Creators:
  United States. Federal Aviation Administration ; National Aerospace Laboratory (Netherlands)
• Subject/TRT Terms:
  Airport Runways Algorithms Braking Feasibility Analysis Friction Real Time Information Runway Overruns Simulation Slipperiness
• Publication/ Report Number:
  DOT/FAA/TC-14/32
• Resource Type:
  Tech Report
• Geographical Coverage:
  United States
• Corporate Publisher:
  United States. Federal Aviation Administration
• Abstract:
  Runway overrun accidents occurring during landings in slippery conditions continue to occur frequently worldwide. After a
  
  number of specific landing overrun accidents in the U.S., the National Transportation Safety Board (NTSB) issued a safety
  
  recommendation to investigate the technical and operational feasibility of outfitting transport category airplanes with equipment
  
  and procedures required to routinely calculate, record, and convey the airplane’s braking ability.
  
  In this context, this study developed an algorithm for real-time onboard runway friction estimation. The algorithm was
  
  demonstrated in a high-fidelity simulation test that applied data and knowledge of detailed aerodynamic and engine models to
  
  represent a specific regional jet. The primary objective was to evaluate the impact of measurement and modeling errors to the
  
  runway friction estimation obtained from the algorithm.
  
  The simulation showed that onboard runway friction estimation can provide an accuracy of approximately ±5%; measuring errors
  
  based on realistic sensor noise and bias. However, to achieve such performance, a fairly precise estimate of instantaneous thrust,
  
  weight, and drag is required. It was noted that 1% of inaccuracy in these quantities translates directly into at least a 1% estimate
  
  error. A representative model of the ground effect is also critical to the estimation accuracy. Nevertheless, errors in the
  
  calculation of aerodynamic lift and pitching moment seemed to be negligible. The results of this study can be further used to
  
  define an operational concept in line with the recommendation of the NTSB.
  
  
• Format:
  PDF
• Collection(s):
  US Transportation Collection
• Main Document Checksum:
  urn:sha256:c5314b276e769765205ea5286a78110b1bab171fe0c617916aa6a66631413eef
• Download URL:
  https://rosap.ntl.bts.gov/view/dot/29057/dot_29057_DS1.pdf
• File Type:
  [PDF - 1.43 MB ]