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  • Applying GN&C Solutions to the Problem of Asteroid Interception for Planetary Defense

    Applying Guidance, Navigation, and Control Solutions to the Problem of Asteroid Interception for Planetary Defense

    An AIAA Distinguished Speaker Lecture, via Zoom

    presented by

    Dr. Nahum Melamed

     Project Leader in the Embedded Control Systems Department of the Guidance and Control Subdivision at The Aerospace Corporation

    Wednesday, January 29th, 12:00-1:00 PM PST

    The impact consequences of Near-Earth Objects (NEO) require proactive measures to eliminate or reduce them when lead times are too short for effective deep space deflection/destruction operation. To expand mitigation beyond deep space, ground-based pre-built interceptors launched minutes before atmospheric entry can respond to detection times from minutes to months before impact with Earth. The disruption of a small NEO prior to its atmospheric entry could potentially eliminate or reduce damage to life and property on the ground by dispersing its kinetic energy over a wider area.

    The Guidance and Control Subdivision at The Aerospace Corporation has applied interceptor techniques to engage an incoming NEO at high altitude minutes before its atmospheric entry. The objective is to disrupt the object and deposit its kinetic energy at a higher altitude and disperse it over a wider footprint on the ground. A Monte Carlo simulation applied fireball statistical properties from a NASA database to correlate flight time and altitude of intercept with interceptor requirements. Preliminary results show that exoatmospheric intercept altitudes are attainable even when detection and launch occur minutes before impact. Local, regional, or national objectives determine the number of systems and response time requirements. Hydrocode modeling demonstrated the amount of disruption caused to the asteroid by several kinetic kill vehicles. Detection technology, terminal guidance capability, disruption analysis, and debris reentry analysis are key areas of future work. 

    Nahum Melamed is a project leader in the Embedded Control Systems Department in the Guidance and Control Subdivision at The Aerospace Corporation. He joined Aerospace in 2003. As a technical lead in Launch Vehicle Software, Dr. Melamed coordinates and guides a team of interdepartmental technical experts, and supports validation and mission readiness certification of the flight software and mission parameters for NASA’s Artemis missions. He conducts planetary defense technical and policy studies, co-chairs planetary defense conferences, serves on organizing committees, and speaks at these venues. He earned a Ph.D. in Aerospace Engineering from Georgia Tech. 

    The presentation will be on Wednesday, January 29th, 2025 from 12:00 PM to 1:00 PM PST via Zoom. The Zoom link for the meeting is below.