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Space / Geometry / Orbital mechanics / Eccentric anomaly / Launch vehicle / Ellipse / True anomaly / Semi-major axis / Orbit / Celestial mechanics / Astrodynamics / Astrology


The Multi-Stage-Lambert Scheme for Steering a Satellite-Launch Vehicle (SLV) Syed Arif Kamal *
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Document Date: 2012-05-18 05:17:25


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City

Washington / DC / Lahore / Karachi / Rawalpindi / Reading / New York / Islamabad / /

Company

Tech Technologies / /

Country

Pakistan / /

Currency

pence / USD / /

Facility

Prentice Hall / Library of Congress / Quaid-é-Azam University / College of Aeronautical Engineering / University of Karachi / Institute of Space Technology / Bahria University / Pakistan Institute of Physics International Conference / /

IndustryTerm

inverse-square-central-force law / elegant algorithm / satellite-launch vehicles / on-board computing system / minimum-energy orbital transfer time / business to business / satellite-launch vehicle / minimum energy orbit / on-board computing time / control law / /

Organization

Institute of Space Technology / Congress / University of Karachi / Karachi / Pakistan Mathematical Society / National Curriculum Revision Committee / College of Aeronautical Engineering / National Center for Physics / Center for Advanced Mathematics and Physics / Pakistan Institute of Physics International Conference / NUST / Department of Mathematics / Visiting Faculty / Higher Education Commission / Quaid-é-Azam University / PAF Academy / Bahria University / Karachi / Department of Aeronautics and Astronautics / /

Person

Addison Wesley / Syed Arif Kamal / /

Position

author / Professor / Dean / /

Product

Satellite / Lambert / /

ProvinceOrState

New York / Massachusetts / /

PublishedMedium

Control Engineering / Advanced Materials / /

Technology

elegant algorithm / elegant Lambert algorithm / Fluid Dynamics / simulation / Lambert algorithm / /

URL

http /

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