Accession Number : ADA137586

Title :   An Iterative Guidance Method for the Large Rocket Launch Vehicle,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH

Personal Author(s) : Han,Z

PDF Url : ADA137586

Report Date : 13 Jan 1984

Pagination or Media Count : 28

Descriptors :   *Guidance, *Adaptive control systems, *Ascent trajectories, Launch vehicles, Rocket propulsion, Artificial satellites, Iterations, Optimization, Control theory, Equations of motion, Translations, China

Subject Categories : Spacecraft Trajectories and Reentry

Distribution Statement : APPROVED FOR PUBLIC RELEASE