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THE EFFECT OF AERODYNAMIC CROSSCOUPLING DURING ROCKET FLIGHT
Author(s): 
Pages: 16-19
Year: Issue:  3
Journal: Aerospace Control

Keyword:  Trajectory calculation Computer aioled design Attitude control Aerodynamic crosseoupling;
Abstract: This paper Presents a linear expression of aerodynamic moment for aerodynamic crosscoupling during rocket flight and an iterative equation of attitude angle is given in which attitude crosscoupling is Considered, These equations canbetter reflcet the relations of the variation of all attitude angles during actical flight process and the original iteration method for one channel is improved. By using this set of equations the trajectory Calculating programs can be perf ormed automatically.
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