Da: liu xing, Nanjing, JS, Cina
paperback. Condizione: New. Paperback. Pub Date: 2017-05-01 Pages: $number Language: Chinese Publisher: Defense Industry Publishing House missile overload control and change trajectory technology mainly introduces differential geometry design method: Missile motion mathematical model ; missile's combined overload control technology; missile's large airspace maneuver technology and small airspace terminal maneuver technology: terminal maneuver and . Codice articolo DP050145
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