F064-B04-021© 2004 The MITRE Corporation. All Rights Reserved.
Potential Impact of EDR on Modeled Arrival Capacity for Closely Spaced
Parallel Runways
Clark R. Lunsford, Wayne W. Cooper, Arthur P. Smith, Anand D. Mundra,
Joseph E. Sherry, Jeffrey A. Tittsworth17 February 2004
2004 The MITRE Corporation. All rights reserved.
© 2004 The MITRE Corporation. All Rights Reserved.F064-B04-021
Outline
• Overview of ATC wake procedure work for NASA Langley Research Center (LaRC)
• Example of an ATC wake procedures • Impact of EDR on lateral wake transport• Relationship of EDR and surface wind• Impact of EDR on capacity increments and delay
benefits
2004 The MITRE Corporation. All rights reserved.
© 2004 The MITRE Corporation. All Rights Reserved.F064-B04-021
Introduction
• Goal is to provide quantitative estimates of benefits for potential WakeVAS concepts or procedures – Enable comparison between concepts – Help NASA select one or two for full development
• Trade off between benefits and development and deployment risks
• Potential concepts analyzed in FY03 for NASA/Langley– Capacity increment over comparable FAA commitments if they
exist; else over current operations– Development and deployment risk analysis (qualitative) will be
addressed in FY04
2004 The MITRE Corporation. All rights reserved.
© 2004 The MITRE Corporation. All Rights Reserved.F064-B04-021
Potential Arrival Procedure Steps Analyzed for Benefits for Closely Spaced Parallel Runways
WakeVAS-PD
WakeVAS-Wx2
WakeVAS-Wx1
WakeVASStep
5b. Use crosswind to allow wake independence for both runways if the crosswind is low enough, judging wake transport of leading cluster aircraft at a level dependent on the weight class of the trailing aircraft, with a tighter safety buffer to the crosswind required
a. Judge wake transport of leading cluster aircraft at a reference level, with a tighter safety buffer to the minimum crosswind required
h
4Use crosswind to allow wake independence for both runways if the crosswind is low enough, judging wake transport of leading cluster aircraft at a level dependent on the weight class of the trailing aircraft, adding a safety buffer to crosswind required
g
3Use crosswind to allow wake independence for both runways if the wind is low enough with the addition of turbulence considerations, adding a safety buffer to the crosswind required
f
Reduce minimum separations between aircraft on parallel approaches to 1 nmi, adding a safety buffer to the crosswind required
e
Use crosswind to allow wake independence for both runways if the crosswind is low enough, judging wake transport of leading cluster aircraft at reference level, adding a safety buffer to crosswind required
d
2Use crosswind to allow wake independence for both runways if the wind is low enough, judging the wake transport of leading wake category aircraft at a reference level, adding a safety buffer to crosswind required
c
1Use crosswind to allow wake independence of upwind runway (all aircraft) , adding a safety buffer to minimum crosswind required
b
Use crosswinds to allow wake independence of upwind runway behind large aircraft; Judge wake transport of leading wake category aircraft at a reference level, add safety buffer to minimum crosswind required
a
Analysis Increment
Potential Procedure stepEvolutionStep
2004 The MITRE Corporation. All rights reserved.
© 2004 The MITRE Corporation. All Rights Reserved.F064-B04-021
Example Procedure for Dependent Approaches to Parallel Runways (Step 3)
Use crosswind to allow wake independence for both runways if the crosswind is low enough, judging wake transport of leading aircraft at a reference level, adding a safety buffer to crosswind required
• Clusters are examples of subdivisions within aircraft type, based on initial wake circulation strength computed using wing span, max landing weight, and minimum approach speed
Lead Cluster Small Large Heavy Lead Cluster Small Large Heavy8 (Small 9.3%) 87 (Large 12.8%) 76 (Large 14.8%) 65 (Large 29.1%) 54 (Large 16.9%) 43 (B757 9.1%) 32 (Heavy 5.1%) 21 (Heavy 2.9%) 1
-- All Winds ---- All Winds ---- All Winds ---- 5-20 kts --
-- All Winds ---- All Winds ---- All Winds ---- All Winds --
-- 0-10 kts ---- 0-10 kts ---- 0-5 kts --
-- No Wind Conditions --
-- All Winds ---- All Winds ---- All Winds ---- 0-15 kts --
1000 ft Runway SeparationDownwind Runway Wake Independence Upwind Runway Wake Independence
Trailing Wake Category Trailing Wake Category
WIND
Cluster 1
1000 ft
Cluster 1Cluster 6
Cluster 3Wake Spacing
1.5 nm
i
1.5 nm
i
2004 The MITRE Corporation. All rights reserved.
© 2004 The MITRE Corporation. All Rights Reserved.F064-B04-021
Low
Mid
Hig
h
Range of EDRs Observed at DFW
Source: Turbulence Climatology at Dallas/Ft. Worth (DFW) Airport--Implications for a Departure Wake Vortex Spacing System, G.H. Perras and T. J. Dasey, November 2000, NASA/L-4.
2004 The MITRE Corporation. All rights reserved.
© 2004 The MITRE Corporation. All Rights Reserved.F064-B04-021
Example of Effect of EDR on Wake Persistence for B757-300 (APA 3.2)
0
50
100
150
200
250
300
350
400
0 60 120 180Time (sec)
Wak
e In
tens
ity
EDR .003
EDR .0001
EDR .0000001
2004 The MITRE Corporation. All rights reserved.
© 2004 The MITRE Corporation. All Rights Reserved.F064-B04-021
DFW Observations of EDR vs. Wind Speed
Wind Speed vs. EDR at DFW
y = 0.0007x1.8308
R2 = 0.7717
y = 0.0002x1.6583
R2 = 0.5347
1.00E-06
1.00E-05
1.00E-04
1.00E-03
1.00E-02
1.00E-01
1.00E+00
0.00 2.00 4.00 6.00 8.00 10.00 12.00 14.00
Wind Speed (m/s)
ED
R
5 Meter40 MeterPower (5 Meter)Power (40 Meter)
June 9, 15, 17, 20 & July 7, 2000NASA data collected for:
Wind Speed vs. EDR at DFW
y = 0.0007x1.8308
R2 = 0.7717
y = 0.0002x1.6583
R2 = 0.5347
1.00E-06
1.00E-05
1.00E-04
1.00E-03
1.00E-02
1.00E-01
1.00E+00
0.00 2.00 4.00 6.00 8.00 10.00 12.00 14.00
Wind Speed (m/s)
ED
R
5 Meter40 MeterPower (5 Meter)Power (40 Meter)
June 9, 15, 17, 20 & July 7, 2000NASA data collected for:
2004 The MITRE Corporation. All rights reserved.
© 2004 The MITRE Corporation. All Rights Reserved.F064-B04-021
EDR and Wake Transport Assumptions in FY03
• Conservative EDR Assumptions (from demise and transport perspective)– Calm wind (0-4.9 kts) has a very low EDR (1.0x10-7)– Medium wind (5-14.9 kts) has a mid-range EDR (1.4x10-3)– High wind (15 kts and greater) has a high EDR (3.0x10-3)
• Modeled wake transport with AVOSS (while wake remained above assumed background turbulence level)
• Applied operational constraints and flight technical error considerations to derive wake transport table for use in procedure exploration
• Delay reductions based on use of historical surface winds and demand for specific airports
2004 The MITRE Corporation. All rights reserved.
© 2004 The MITRE Corporation. All Rights Reserved.F064-B04-021
Example of AVOSS Modeled B757-300 Wake Transport with Wind (APA 3.2)
0
100
200
300
400
500
600
700
0 60 120 180Time (sec)
Late
ral T
rans
port
(m)
Wind 20 kts EDR .003
Wind 0 kts EDR .0000001
2004 The MITRE Corporation. All rights reserved.
© 2004 The MITRE Corporation. All Rights Reserved.F064-B04-021
Simulation Mechanics
EXCEL Model@Risk RandomInput Generator
Run Parameters
12
34
@Risk DataAccumulator
@RiskSimulationController
ComplexLogic
Visual BasicCode
Visual BasicCode
Batch ModeController
2004 The MITRE Corporation. All rights reserved.
© 2004 The MITRE Corporation. All Rights Reserved.F064-B04-021
Comparison of Capacity Results
Seattle Arrival Rate Comparison
0.0
2.0
4.0
6.0
8.0
10.0
12.0
14.0
16.0
0 5 10 15 20
Crosswind
Incr
ease
ove
r S
ing
le R
un
way
FAA Increase
S1 Increase
S2 Increase
S3 Increase
S5 Increase
San Francisco Arrival Rate Comparison
0.0
2.0
4.0
6.0
8.0
10.0
12.0
14.0
16.0
18.0
0 5 10 15 20
Crosswind
Incr
ease
ove
r S
ing
le R
un
way
FAA Increase
S1 Increase
S2 Increase
S3 Increase
S5 Increase
• Several ATC wake procedures were analyzed (Step 1 – Step 5 with increasing technology needs)
• Higher than assumed EDR will increase the wind cases where runways can be run wake independent, moving these curves up, increasing the increment in capacity
• Lower than assumed EDR will decrease the opportunities to run the procedure and decrease the capacity increment
2004 The MITRE Corporation. All rights reserved.
© 2004 The MITRE Corporation. All Rights Reserved.F064-B04-021
Airport Average Arrival Delay Reduction Per Day (with winds and current demand)
• This chart shows the estimated average delay reduction in hours per day when moving from current arrival capacity to that of the FAA baseline, plus each of the four procedures
• Step 1 shows significant benefits at airports with runway centerline separation less than 1000 ft
• Step 2 provides a small improvement over Step 1 and the FAA baseline results
• Steps 3 and 5 appear to show minimal improvements over Step 2 with respect to delay for current demand
• Considers surface winds only and demand for January-December 2002
Average Daily Delay Benefits by Procedure For Airport
0
2
4
6
8
10
12
14
LAX SFO SEA EWR MEM CLE STL PHL BOS
Del
ay (
in h
ou
rs)
FAA Baseline Step 1 Step 2 Step 3 Step 5
2004 The MITRE Corporation. All rights reserved.
© 2004 The MITRE Corporation. All Rights Reserved.F064-B04-021
Acknowledgements
• Dave Rutishauser at NASA LaRC for sharing AVOSS expertise and providing extensive AVOSS wake track data sets (72 aircraft types, 6 winds, 3 EDRs)
• Burnell McKissick at NASA LaRC for providing DFW wind and EDR data observations
• Wayne Bryant at NASA LaRC for guidance in ATC procedure analysis and downselect
2004 The MITRE Corporation. All rights reserved.