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Science / Aerospace engineering / Orbital mechanics / Orbit / Control theory / Global Positioning System / Technology / Celestial mechanics / Military science


Advanced Guidance Algorithms for Spacecraft Formation-keeping∗ Michael Tillerson† and Jonathan P. How‡ Space Systems Laboratory Massachusetts Institute of Technology Abstract
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Document Date: 2011-06-05 16:48:17

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City

Breckenridge / London / Chicago / /

Company

A.I. Solutions / Enhanced Autonomy Technologies / Eccentric Orbits / Space Systems Laboratory / Rel Dyn LP / /

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Facility

Jonathan P. How‡ Space Systems Laboratory / Massachusetts Institute of Technology / /

IndustryTerm

control algorithms / guidance algorithm / virtual satellite / feasible solution / closed-form solutions / closed form solutions / formation-keeping guidance algorithms / satellite thrusters / satellite acts / guidance algorithms / imaging / form-solutions / satellite position / feasible solutions / /

Organization

National Aeronautics and Space Administration / Air Force / Massachusetts Institute of Technology / Orion-Emerald mission / Air Force Research Laboratory Space Vehicles Directorate / /

Person

Michael Tillerson / Jonathan P. How / /

Position

model for developing trajectories / †Research Assistant / central coordinator / LP controller / controller / Associate Professor / /

Product

Orion / PROJECT ORION / /

ProgrammingLanguage

J / C / /

ProvinceOrState

Massachusetts / Colorado / /

PublishedMedium

the International Journal / the Orion / /

Technology

radiation / guidance algorithm / LP algorithm / control algorithms / GPS / 3.2 Algorithm / formation-keeping guidance algorithms / simulation / guidance algorithms / /

URL

http /

SocialTag