Presentation is loading. Please wait.

Presentation is loading. Please wait.

The National Airspace System as a Cyber-Physical System Hamsa Balakrishnan Massachusetts Institute of Technology Joint work with: Diana Michalek, Harshad.

Similar presentations


Presentation on theme: "The National Airspace System as a Cyber-Physical System Hamsa Balakrishnan Massachusetts Institute of Technology Joint work with: Diana Michalek, Harshad."— Presentation transcript:

1 The National Airspace System as a Cyber-Physical System Hamsa Balakrishnan Massachusetts Institute of Technology Joint work with: Diana Michalek, Harshad Khadilkar, Hanbong Lee, Ioannis Simaiakis and Varun Ramanujam NSF−UC Berkeley−MIT ActionWebs Summer Meeting July 23, 2010

2 Research objectives Increase efficiency of operations Multi-objective control techniques for balancing tradeoffs Decrease fuel burn and environmental impact Increase operational robustness in the presence of weather More flexible and dynamic trajectories More decentralized decision-making The use of onboard sensing in ActionWebs, combined with the development of hybrid systems models of aircraft trajectories can help us achieve these objectives

3 Motivation In 2007, domestic air traffic delays [JEC, US Senate]  Had a $41 billion impact on the US economy  Cost airlines an additional $1.6 billion in fuel costs  Consumed an additional 740 million gallons of jet fuel  Released an additional 7.1 million tons of CO 2 into the atmosphere In 2007, aircraft in the U.S. spent over 63 million minutes taxiing in to their gates, and over 150 million minutes taxiing out for departure [FAA] Taxiing aircraft burn fuel, and contribute to surface emissions of CO 2, hydrocarbons, NOx, SOx and particulate matter  An estimated 6 million tons of CO 2, 45,000 tons of CO, 8,000 tons of NOx and 4,000 tons of hydrocarbons are emitted annually by aircraft taxiing out In Europe, aircraft are estimated to spend 10-30% of their time taxiing A short/medium range A320 expends as much as 5-10% of its fuel on the ground [Airbus]

4 Boston Logan airport, 1830hrs, 01/06/2010

5 Efficient and equitable arrival/departure runway scheduling Given a set of flights with estimated arrival times at the airport, the aircraft need to be sequenced into the landing (takeoff) order, and the landing (takeoff) times need to be determined  Minimum separation between operations for wake avoidance (wt. class dependent) (Safety)  Currently FCFS; resequencing could increase throughput (Efficiency) SeparationHL/B757S H96157196 L/7576069131 S606982 Trailing a/c Leading a/c Separation in seconds HSHS 196 s60 s 196 s 452 s SH 60 s 96 s S 60 s H 216 s *[Dear 1976, Psaraftis 1980, Garcia 1990, Volckers 1990, Neuman and Erzberger 1991, Venkatakrishnan, Barnett and Odoni 1993, Trivizas 1998, Beasley 2000, Anagnostakis 2001, Carr 2004]  Fairness: Constrained Position Shifting* FCFS… … … … k = 2 678910

6 Runway scheduling under Constrained Position Shifting (CPS) [Balakrishnan and Chandran AIAA GNC 2006; Operations Research (2010, to appear)] Key result: We have proved that this is not true Basic idea: We propose a way to represent solution space as a network whose size is linear in the number of aircraft Key result: We have proved that this is not true Basic idea: We propose a way to represent solution space as a network whose size is linear in the number of aircraft [USA/Europe ATM R&D Seminar 2007; Amer. Control Conf. 2007, Amer. Control Conf. 2008, Proceedings of the IEEE (2008)] Well-studied problem, using various (mostly heuristic) approaches Challenge: Scheduling under CPS has been conjectured to have exponential computational complexity in the number of aircraft [Carr 2004] Various interesting extensions can be solved in (pseudo-)polynomial time as shortest-path problems on variations of this network  Multiple objectives: Average delay, max. delay, sum of delay costs, fuel costs, operating costs, robustness to uncertainties, etc.  Evaluation of tradeoffs between multiple objectives

7 CPS network Size of network is linear in the number of aircraft and exponential in k (≤3) Easy to incorporate arrival time windows and precedence constraints Precedence constraints make problem easier to solve n = 6, k = 1 Length = (2 k +1) Length = min(Stage#,2 k +1) # of arcs [Balakrishnan and Chandran, AIAA GNC 2006; Operations Research (2010, to appear)]

8 Tradeoffs between throughput and delay costs Randomly generated sequence, 40% Heavy, 40% Large, 20% Small Delay costs of Heavy and Large are 9x (Delay cost of Small aircraft) This gain in throughput comes at a very high cost [Lee and Balakrishnan, Proceedings of the IEEE, 2008] throughput gain increase in cost

9 Is speeding up necessarily a good idea? Accelerating from the nominal speed requires more fuel However, speeding up the first aircraft in a sequence may decrease the delay incurred by subsequent aircraft  Concept of Time advance [Neuman and Erzberger 1991, Lee and Balakrishnan ACC 2008]

10 Evaluating the benefits of Time Advance Total estimated fuel cost vs. allowable time advance [Lee and Balakrishnan, Proceedings of the IEEE, 2008]

11 Modeling the taxi-out process

12 Queuing network model of the taxi-out process Model inputs (ASPM database)  Pushback schedules  Gate assignments  Runway configurations  Weather conditions Desired outputs  Taxi-out time for each flight  Level of congestion on airport surface  Loading on departure queues

13 Estimating taxi-out time Taxi-out time expressed as  =  unimpeded +  taxiway +  dep.queue  Unimpeded taxi-out time (  unimpeded ) dominates when the number of aircraft on the surface is low  Departure queue wait time (  dep.queue ) dominates when the number of departures on the surface is high  Taxiway congestion term (  taxiway ) is important under medium traffic conditions Parameter estimation:  Unimpeded taxi-out time  Departure throughput saturation  Runway service process [Simaiakis and Balakrishnan, AIAA GNC, 2009]

14 Improvement through including taxiway congestion term Assume  taxiway =  R ( t ) R ( t ) is the number of aircraft on ramps and taxiways Choose  for best parameter fit Without taxiway congestion term With taxiway congestion term [BOS; 4L,4R|4L,4R,9; VMC] [Simaiakis and Balakrishnan, AIAA GNC, 2009]

15 Model validation: departure throughput Model validated on 2008 data Without taxiway congestion term With taxiway congestion term [BOS; 4L,4R|4L,4R,9; VMC] [Simaiakis and Balakrishnan, AIAA GNC, 2009]

16 Taxi times as a function of congestion High (N ≥ 17) Medium (9 ≤N ≤16) Low (N ≤ 8) [Simaiakis and Balakrishnan, AIAA GNC, 2009]

17 Prediction of taxi-out times min [Simaiakis and Balakrishnan, AIAA GNC, 2009]

18 One potential strategy: “N-Control” Conceptually simple: Limit the buildup of queues on the airport surface by controlling the pushback times of aircraft  If number of aircraft in movement area > N ctrl Add any departing aircraft that requests clearance to a virtual departure queue, unless there is an aircraft waiting to use the gate, in which case, clear departure for pushback  If number of aircraft in movement area ≤ N ctrl Clear aircraft in virtual departure queue for pushback in FCFS order, unless there is a flight waiting to use the gate of an aircraft in the virtual departure queue, in which case, clear departure for pushback Model can be used to evaluate surface traffic management strategies Pushback requests Pushback clearances Departure queue Departure throughput (Virtual) pushback queue for N-control Ramp and taxiway interactions Runway

19 Evaluating delay-emissions tradeoffs

20 Effect of stopping and starting while taxiing Potential fuel burn impact from stopping on the surface No significant impact

21 Effect of stopping and starting while taxiing Impact depends on pilot actions No significant change in thrust setting thrust setting (%)

22 Using CFDR data to estimate impact of different taxi profiles ICAO emissions databank assumes that aircraft taxi at a constant thrust setting of 7% Using CFDR data (from Swiss Air) corresponding to taxi profiles of various aircraft, we  Developed a regression model for fuel burn, that considers the baseline fuel burn and the impact of stop-start events Stop-start impact: Estimate of the form “The extra fuel burn from a start-stop event is equivalent to x additional minutes of taxi time”  Developed a (linear) regression model between fuel burn and thrust settings  Conducted above analysis for 9 aircraft types Fuel burn / √Temp = Baseline fuel burn rate  (taxi time) + (Stop-start impact)  (# of stop-start events)

23 CFDR estimates vs. ICAO fuel burn rates 9.9% 8.8% 1.6% 7.4% 4.0% 6.3% 27.4% 4.1% 5.9% [Khadilkar, Balakrishnan & Reynolds, working paper, 2010] Labels indicate thrust settings; ICAO assumes 7% constant thrust during taxi.

24 Results of CFDR analysis Taxi time is by far the dominating factor in determining taxi fuel burn Impact of stops and turns appears to be due to the increase in taxi time, rather than due to a significant change in the fuel burn rate  The majority of fuel consumed during stops appeared to be due to the additional time, rather than the application of breakaway power; the exact estimates varied (depending on aircraft type) from 3%- 15% of the average fuel burn during a stop corresponding to the breakaway In the data set considered (mostly from European airports), each stop appeared to add on average 2 min to the taxi time, while each turn added on average 20 seconds [Khadilkar, Balakrishnan & Reynolds, working paper, 2010]

25 Comparison of CFDR and surface surveillance data Hybrid estimation to filter surface tracks Compare time spent in different taxi modes ASDE-X data is only from BOS; CFDR is from mostly European and a few US airports

26 Predictive model for routing Can we build a model of the airport surface that allows us to predict taxi times and recommend taxi routes? Mean error: -32 sec, stdev: 141 sec At first node in path Mean error: -4sec, stdev: 121 sec At second node in path Take-offs from Node 7

27 Predictive model for routing

28

29 Mitigating the impact of weather on air traffic operations Objectives:  More flexible and dynamic trajectories  Increase efficiency of operations  Increase operational robustness in the presence of weather Routing flexibility increases capacity E.g., can we find a route within B km of original route that does not pass through weather Forecast Actual B [Michalek and Balakrishnan, ATM R&D Seminar 2009]

30 Dynamic fix relocation: 60-min ahead Pilots typically assumed to avoid Level 3+ weather

31 Dynamic fix relocation: 60-min ahead Pilots typically assumed to avoid Level 3+ weather

32 Dynamic fix relocation: 60-min ahead Pilots typically assumed to avoid Level 3+ weather

33 Dynamic fix relocation: 60-min ahead Pilots typically assumed to avoid Level 3+ weather

34 Dynamic fix relocation: 60-min ahead Pilots typically assumed to avoid Level 3+ weather

35 Dynamic fix relocation: 60-min ahead Pilots typically assumed to avoid Level 3+ weather

36 Dynamic fix relocation: 60-min ahead Pilots typically assumed to avoid Level 3+ weather

37 Dynamic fix relocation: 60-min ahead Pilots typically assumed to avoid Level 3+ weather

38 Resectorization and rerouting/relocating fix Forecast Observed WHINZ CADIT LAGRANGE BRAVS SINCA DOOLY GEETK ROME WHINZ CADIT LAGRANGE BRAVS SINCA DOOLY GEETK ROME New Sector boundary Old sector boundary New Fix Old Fix Legend Multi-objective optimization: Maximize probability of fixes being open; minimize movement of sector boundary; minimize deviation of route from procedural route; try to keep all sectors open Pilots typically assumed to avoid Level 3+ weather

39 Summary statistics of resectorization (fix/route relocation) Note that these metrics do not reflect the probability with which fix was predicted to be open. 77% 71% 85% 72% 95% 88% 86% 85% 0% 7% 4% 5% 3% [Michalek and Balakrishnan, CDC 2010]

40 Summary statistics of resectorization (fix/route relocation) [Michalek and Balakrishnan, CDC 2010]

41 Pilot behavior Of course, pilots do occasionally penetrate weather today Can provide additional flexibility Can we identify the factors that determine their behavior? “3 Weather days” “Really bad weather day”

42 Conclusions Air transportation system presents many important problems that require the development of CPS methodologies Solutions have the potential to increase system efficiency (reduce delays), robustness and energy efficiency (reduce fuel burn), and decrease environmental impact Key objectives should include  More dynamic, flexible trajectories (and system structure)  Multi-objective control and balancing of tradeoffs  More decentralized decision-making

43


Download ppt "The National Airspace System as a Cyber-Physical System Hamsa Balakrishnan Massachusetts Institute of Technology Joint work with: Diana Michalek, Harshad."

Similar presentations


Ads by Google