Aisha Bowe

Washington, District of Columbia, United States Contact Info
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Aisha Bowe is a former NASA rocket scientist, 2X Founder, Blue Origin astronaut, and host…

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Publications

  • An Approach for Balancing Delay and Fuel Burn in Separation Assurance Automation

    American Institute of Aeronautics and Astronautics (AIAA)

    A conflict resolution algorithm is introduced that enables a user to specify the degree to which fuel economy is prioritized relative to airborne delay, analogous to the “cost index" setting in flight management computers. Fast-time simulations of current-day traffic levels in two regional airspaces under nominal weather conditions are simulated to evaluate the benefit of modifying a conflict resolution algorithm to select resolution maneuvers based on minimum cost. The study employs the use of…

    A conflict resolution algorithm is introduced that enables a user to specify the degree to which fuel economy is prioritized relative to airborne delay, analogous to the “cost index" setting in flight management computers. Fast-time simulations of current-day traffic levels in two regional airspaces under nominal weather conditions are simulated to evaluate the benefit of modifying a conflict resolution algorithm to select resolution maneuvers based on minimum cost. The study employs the use of a parameter to represent the relative importance of fuel burn price to delay price. Additionally, the price of fuel burn and delay relative to one another is varied from the nominal in order to illustrate the differences in the algorithmic behavior should the delay or fuel price increase. Results show the lowest total operational cost occurs when the relative importance of delay to fuel burn price is equally weighted. Overall, minimizing fuel burn when selecting resolutions based on cost results in a lower operational cost than minimizing delay. The sensitivity of total operational cost to resolution types is presented. Implications of these findings for advanced separation assurance concepts are discussed.

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  • Robust Conflict Detection and Resolution around Top of Descent

    American Institute of Aeronautics and Astronautics

    One of the complicating factors when detecting and resolving aircraft-to-aircraft conflicts is the presence of uncertainty, which can cause conflicts to be detected without sufficient time to resolve them. Previous work by the authors has shown this situation occurs most often when the uncertainties affect the trajectory of an aircraft near or in its descent phase. This paper attempts to address this issue by exploring a pair of enhanced vertical conflict detection ranges (buffers) for…

    One of the complicating factors when detecting and resolving aircraft-to-aircraft conflicts is the presence of uncertainty, which can cause conflicts to be detected without sufficient time to resolve them. Previous work by the authors has shown this situation occurs most often when the uncertainties affect the trajectory of an aircraft near or in its descent phase. This paper attempts to address this issue by exploring a pair of enhanced vertical conflict detection ranges (buffers) for descending aircraft that could provide enough coverage to catch all potential losses near and during descent for multiple types of uncertainty while minimizing the increase in the rate of false alerts. The paper examines uncertainties in the prediction of wind speed, cruise speed, descent speed, top-of-descent location, and the combination of all of those uncertainties plus uncertainty in aircraft weight prediction. The vertical conflict detection buffers are designed to improve performance of the conflict prediction and resolution tools near or after the top-of-descent, so the focus will be on conflicts involving at least one aircraft that is an arrival. These vertical conflict detection buffers should also be tunable to different levels of trajectory prediction accuracy. Therefore, for a known range of uncertainty, there should exist a minimum vertical buffer that will detect all of the conflicts that could occur near or after the top-of-descent. Therefore a second goal of this work is to show that these buffers can be adapted to fit a given range of uncertainty, so that as trajectory predictions improve, the vertical conflict detection ranges can be decreased to reduce the number of false alerts while maintaining safe separation. Finally, the impact of these vertical detection buffers on the conflict resolution process is examined. With buffers tuned to the amount of trajectory prediction error, the total delay as a function of trajectory prediction error is presented.

    Other authors
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  • A Fuel-Efficient Conflict Resolution Maneuver for Separation Assurance

    National Aeronautics and Space Administration NASA/TM-2012-216009

    This experiment evaluates the benefit of augmenting a conflict detection and resolution algorithm to consider a fuel-efficient, Variable Speed Direct-To maneuver when resolving a given conflict based on either minimum fuel burn or minimum delay. Twelve conditions were tested in fast-time simulation conducted in three airspace regions with mixed aircraft types and nominal traffic. Inclusion of this maneuver had no appreciable effect on the ability of the algorithm to safely detect and resolve…

    This experiment evaluates the benefit of augmenting a conflict detection and resolution algorithm to consider a fuel-efficient, Variable Speed Direct-To maneuver when resolving a given conflict based on either minimum fuel burn or minimum delay. Twelve conditions were tested in fast-time simulation conducted in three airspace regions with mixed aircraft types and nominal traffic. Inclusion of this maneuver had no appreciable effect on the ability of the algorithm to safely detect and resolve conflicts. Cumulative fuel burn savings were significantly higher when selecting resolutions based on minimum fuel burn; average delay per resolution was only marginally higher.


    Other authors
    • Confesor Santiago
  • Evaluation of a Fuel Efficient Maneuver For Conflict Resolution

    NASA

    Automated separation assurance algorithms are envisioned to play an integral role in accommodating the forecasted increase in demand of the National Airspace System. Developing a robust, reliable, air traffic management system involves safely increasing efficiency and throughput while considering the potential impact on users. This experiment seeks to evaluate the benefit of
    augmenting a conflict detection and resolution algorithm to consider a fuel efficient, Zero-Delay Direct-To…

    Automated separation assurance algorithms are envisioned to play an integral role in accommodating the forecasted increase in demand of the National Airspace System. Developing a robust, reliable, air traffic management system involves safely increasing efficiency and throughput while considering the potential impact on users. This experiment seeks to evaluate the benefit of
    augmenting a conflict detection and resolution algorithm to consider a fuel efficient, Zero-Delay Direct-To maneuver, when resolving a given conflict based on either minimum fuel burn or minimum delay. A total of eight conditions were tested in a fast-time simulation conducted in two airspace regions with mixed aircraft types and light weather. Results show that inclusion of this maneuver has no appreciable effect on the ability of the algorithm to safely detect and resolve conflicts. The results further suggest that enabling the Zero-Delay Direct-To maneuver significantly increases the cumulative fuel burn savings when selecting resolution based on minimum fuel burn while marginally increasing the average delay per resolution.

    Other authors
    • Confesor Santiago
    See publication
  • Relative Significance of Trajectory Prediction Errors on an Automated Separation Assurance Algorithm

    Air Traffic Management Research and Development Seminar

    Trajectory prediction is fundamental to automated separation assurance. Every missed alert, false alert and loss of separation can be traced to one or more errors in trajectory prediction. These errors are a product of many different sources including wind prediction errors, inferred pilot intent errors, surveillance errors, navigation errors and aircraft weight estimation errors. This study analyzes the impact of six different types of errors on the performance of an automated separation…

    Trajectory prediction is fundamental to automated separation assurance. Every missed alert, false alert and loss of separation can be traced to one or more errors in trajectory prediction. These errors are a product of many different sources including wind prediction errors, inferred pilot intent errors, surveillance errors, navigation errors and aircraft weight estimation errors. This study analyzes the impact of six different types of errors on the performance of an automated separation assurance system composed of a geometric conflict detection algorithm and the Advanced Airspace Concept Autoresolver resolution algorithm. Results show that, of the error sources considered in this study, top-of-descent errors were the leading contributor to missed alerts and failed resolution maneuvers. Descent-speed errors were another significant contributor, as were cruise-speed errors in certain situations. The results further suggest that increasing horizontal detection and resolution standards are not effective strategies for mitigating these types of error sources.

    Other authors
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  • Selecting Conflict Resolution Maneuvers Based on Minimum Fuel Burn

    Institute of Electrical and Electronics Engineers (IEEE)

    The effects of selecting conflict resolution maneuvers based on minimum delay are compared to resolution selection based on minimum fuel burn. The algorithm used in this study is designed to support an automated separation assurance capability for next generation air traffic management systems. The algorithm resolves detected conflicts that are projected to be between three and twenty minutes prior to loss of separation. A total of nine fast-time simulations were conducted, each representing…

    The effects of selecting conflict resolution maneuvers based on minimum delay are compared to resolution selection based on minimum fuel burn. The algorithm used in this study is designed to support an automated separation assurance capability for next generation air traffic management systems. The algorithm resolves detected conflicts that are projected to be between three and twenty minutes prior to loss of separation. A total of nine fast-time simulations were conducted, each representing thirty six hours of traffic on a "low weather," high volume day with mixed aircraft types, flight phases and conflict geometries. The test matrix varied airspace region and resolution selection criteria. System-wide effects such as the number of conflicts, fuel burn, delay, and maneuver type are analyzed and compared to the same metrics when maneuvers are selected based on delay. When selecting resolutions based on fuel burn, the cumulative fuel burn of the system decreases by 27% and the delay increases by 25% when compared to resolutions selected based on minimum delay. Results indicate that speed maneuvers are the most efficient when selecting resolutions based on minimum fuel burn. Horizontal and vertical maneuvers were executed with similar frequency when comparing delay and fuel burn.

    Other authors
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Projects

  • Unmanned Aircraft Systems Integration in the National Airspace

    There is an increasing need to fly Unmanned Aircraft Systems (UAS) in the National Airspace System (NAS) to perform missions of vital importance to national security and defense, emergency management, science, and to enable commercial applications. One example of this is the use of the Predator UAS by the Department of Homeland Security to fly along our nation's borders.

    UAS are unable to routinely access the NAS today due to a lack of sense-and-avoid concepts and technologies that are…

    There is an increasing need to fly Unmanned Aircraft Systems (UAS) in the National Airspace System (NAS) to perform missions of vital importance to national security and defense, emergency management, science, and to enable commercial applications. One example of this is the use of the Predator UAS by the Department of Homeland Security to fly along our nation's borders.

    UAS are unable to routinely access the NAS today due to a lack of sense-and-avoid concepts and technologies that are interoperable with the NAS, robust communication technologies robust human systems integration, and standardized safety and certification guidelines.

    To date, the primary user of UAS has been the military. For all applications, the current federal aviation regulations are built upon the condition of a pilot being in the aircraft. There exist few, if any, regulations specifically addressing UAS. The technologies and procedures to enable seamless operation and integration of civil UAS in the NAS need to be developed, validated and employed by the Federal Aviation Administration through rule making and policy development.

    The goal of the UAS Integration in the NAS Project is to contribute capabilities that reduce technical barriers related to the safety and operational challenges associated with enabling routine UAS civil access to the NAS.

    Other creators
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Honors & Awards

  • Woman of the Year in Technology

    National Coalition of 100 Black Women, Inc., Silicon Valley Chapter

    The National Coalition of 100 Black Women, Inc., Silicon Valley Chapter continues this annual acknowledgment in order to highlight the achievements of African-American women and their positive contributions to the community. More specifically, their desire is to cultivate a sense of cultural and professional pride in underserved and underrepresented children by highlighting the accomplishments of women who have demonstrated excellence in the areas of technology, education and advocacy.

  • Special Recognition

    Black Engineer of the Year

    The Black Engineer of the Year Awards are one of the most prestigious and competitive honors in science, engineering and technology management. In the BEYA twenty-seven year history, thousands have been nominated but less than 700 have achieved the distinction of being a Black Engineer of the Year honoree.

  • NASA FIRST Leadership Development Program

    NASA

    Competitively selected to participate in the 2012 class of NASA’s Foundation of Influence, Relationships, Success and Teamwork (FIRST) , a one-year agency-wide leadership development program for civil servants designed to enhance personal effectiveness, business acumen, and leadership skill.

  • NASA Ames Engineering Honor Award

    NASA Ames Reseach Center

    Competitive, peer reviewed award given to those who demonstrate engineering excellence. Only three engineers from NASA Ames were selected to receive the award in 2012.

  • NASA Equal Employment Oppourtunity Medal

    NASA

    This prestigious NASA medal is awarded to both Government and non-Government individuals for outstanding achievement and material contribution to the principles and goals of NASA's Equal Employment Opportunity, Diversity, and Inclusion Programs, either within the Government or within community organizations or groups.

  • 21st Century Trailblazer in Aerodynamics and Aviation

    National Society of Black Engineers

    The 21st Century Trailblazers in Aerospace recognizes entry level to mid career engineers who show high promise to provide significant technological contributions to the United States in the aerospace field. These individuals are engaged in important work and are active contributors to civil, military, or commercial aerospace products

  • Outstanding Technical Contribution

    National Society of Black Engineers

    This award recognizes the most innovative technical content within the NSBE Aerospace Systems conference. Aisha Bowe, was awarded "Outstanding Technical Contribution" for her paper, "Evaluation of a Fuel-Efficient Aircraft Maneuver for Conflict Resolution." The paper, co-authored with Confesor Santiago, was considered the "the outstanding paper in terms of quality, innovation and experimentation

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