Výsledky vyhledávání - "HYBRID GUIDANCE ALGORITHMS"

Orbit Selection and EKV Guidance for Space-Based ICBM Intercept

Autoři: Aydin, Ahmet T. NAVAL POSTGRADUATE SCHOOL MONTEREY CA

Přispěvatelé: Aydin, Ahmet T. NAVAL POSTGRADUATE SCHOOL MONTEREY CA

Zdroj: DTIC AND NTIS

Témata: Antimissile Defense Systems, Guided Missile Traj, Accuracy and Ballistics, Surface-launched Guided Missiles, Navigation and Guidance, Spacecraft Trajectories and Reentry, BOOST PHASE, MATHEMATICAL PREDICTION, INTERCEPT TRAJECTORIES, SPACE BASED, BALLISTIC MISSILE INTERCEPT SYSTEMS, INTERCONTINENTAL BALLISTIC MISSILES, ALGORITHMS, COMPUTERIZED SIMULATION, NORTH KOREA, PROPORTIONAL NAVIGATION, CHINA, KILL VEHICLES, INTERCEPTOR SPACECRAFT, MISS DISTANCE, IRAN, EXOSPHERE, LIMITATIONS, THESES, THREATS, MILITARY REQUIREMENTS, GUIDED MISSILE TRAJECTORIES, ORBIT SELECTION, HYBRID GUIDANCE ALGORITHMS, SPACE-BASED MISSILE DEFENSE

Popis souboru: text/html

Relation: http://www.dtic.mil/docs/citations/ADA439839

Dostupnost: http://www.dtic.mil/docs/citations/ADA439839
http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=ADA439839