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John R. Henderson

Researcher at Lawrence Livermore National Laboratory

Publications -  13
Citations -  131

John R. Henderson is an academic researcher from Lawrence Livermore National Laboratory. The author has contributed to research in topics: Atmospheric model & Collision. The author has an hindex of 6, co-authored 13 publications receiving 120 citations.

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Patent

Scheduler for monitoring objects orbiting earth using satellite-based telescopes

TL;DR: In this paper, the ground-based controller determines when the target objects of interest will be near enough to a satellite for that satellite to collect an image of the target object based on an initial orbital model for the targets.
Proceedings ArticleDOI

Modeling of adaptive-optics-based free-space communications systems

TL;DR: In this article, a wave-optics based simulation code written to model a complete free space laser communications link, including a detailed model of an adaptive optics compensation system, is presented, where the phase of a communications laser beam is corrected, after it propagates through a turbulent atmosphere.
Journal ArticleDOI

Use of Landsat 5 for Change Detection at 1998 Indian and Pakistani Nuclear Test Sites

TL;DR: Landsat 5 data on the 1998 Indian and Pakistani tests are used here to demonstrate that there are detectable changes in surface features which might be used to localize an underground nuclear test and to develop change detection techniques specific to the use of satellite data to support a CTBT on-site inspection.
Proceedings ArticleDOI

Intelligent sensor tasking for space collision mitigation

TL;DR: In this paper, the authors explore a new paradigm for improving satellite conjunction analysis by obtaining more precise orbital information only for those objects that pose a collision risk greater than a defined threshold to a specific set of satellites during a specified time interval.
Patent

Modeling the long-term evolution of space debris

TL;DR: In this paper, a space object modeling system that models the evolution of space debris is provided, which simulates interaction of space objects at simulation times throughout a simulation period, including a propagator that calculates the position of each object at each simulation time based on orbital parameters.