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Bar-Shalom, P.

Willett, and X. Xiong and P.


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Estimation and Prediction of Ballistic Missile Trajectories | RAND

Bar-Shalom, and P. Aly, R. Fouly, and H. Blom and Y. Yuan, Y. Willett, E. Mozeson, S.


  1. USA - Ballistic projectile trajectory determining system - Google Patents.
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  4. Optimal Guidance Law Design for Interception of Ballistic Missiles during the Boost Phase?
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  6. Kalman filter - Wikipedia?
  7. It encapsulates our collaboration with the Missile Defense Agency," Montgomery said. The company used a surrogate commercial aircraft that was outfitted with DAS. The radar produced and communicated three-dimensional trajectory data at the Pacific Missile Range Facility in Hawaii to the ballistic missile test bed in San Diego, CA, he said. The DAS ground-based sensor autonomously detected a rocket during the experiment and categorized the event as a ballistic missile launch.

    Employment, combat readiness, and support of current and future aerospace forces. Two years later, the project's contract and personnel were separated from Douglas to form a new, private nonprofit institution to improve public policy through research and analysis for the public welfare and security of the United States-the foundation of what is known today as RAND.

    Jeffrey A. Isaacson MIT PhD Theoretical Physics is a senior physical scientist at Rand whose research interests include ballistic missile defense, conventional weapons proliferation, and longrange planning.

    Air Drag Effects on the Missile Trajectories

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    Optimal Guidance Law Design for Interception of Ballistic Missiles during the Boost Phase

    To examine the capabilities satellites can bring to bear in a theater missile defense TMD environment, the authors describe a methodology, based on Kalman filtering, for the estimation and prediction of ballistic missile trajectories and then apply the methodology to a notional theater ballistic missile. One useful application is in estimating the uncertainty associated with the location of a missile launch.

    Determining missile location uncertainty at any point along the trajectory is another application. Filters optimized for random errors alone as well as random plus bias errors are outlined.