Affiliation:
1. Second Artillery Engineering University
Abstract
In order to further improve the performance of the air launched ballistic missile, a full range of air launched method had been given. For the full range launch program faced initial roll angle and initial lateral speed problem, researched the initial roll angle control mode processing technology in the virtual body coordinates and correct the lateral initial velocity method used angle of sideslip flight procedures. Given the ballistic flight simulation Using the proposed method and technology, and verified the feasibility of the ballistic missile program of all-round air launched.
Publisher
Trans Tech Publications, Ltd.
Reference5 articles.
1. M arti Sarigul, Nesrin Sarigul-Kliji: Trade Studies for Air Launching a Small Launch Vehicle from a Cargo Aircraft [J]. AIAA 2005-0621.
2. Marti Sarigul-Klijn, Nesrin Sarigul-Klijn: Gravity Air Launc h ing of Earth-to-Orbit Space Vehicles [J]. AIAA 200 6 - 7256.
3. Zhang DengCheng: Towed reused launch vehicle flight dynamics [D]. Xi'an: Northwestern Polytechnical University, 2005. 9.
4. He Ming: Studies on Initial Trajectory Stabilization Methods for Internal Air-Launched Rocket [D]. Xi'an: Northwestern Polytechnical University, 2010, 3.
5. Xiao LongXu, Wang ShunHong, Wei ShiHui, ed. Ground-to-ground ballistic missile Guidance technology and hit accuracy [M] Beijing: National Defense Industry Press, (2009).