作者
Chris Porter, Casey Fagley, John Farnsworth, Jürgen Seidel, Thomas McLaughlin
发表日期
2014/7
期刊
AIAA journal
卷号
52
期号
7
页码范围
1430-1440
出版商
American Institute of Aeronautics and Astronautics
简介
The flowfield around an axisymmetric forebody at a high angle of attack () produces a significant side force. This side force results from an asymmetric pressure distribution around the body due to an asymmetric vortex configuration. Numerical studies of open-loop control using mass blowing slots near the tip of the model have shown a proportional response of the side force over a range of momentum coefficient amplitudes. From the open-loop simulations, a prediction-error minimization method was employed to formulate a linear time-invariant model, which captured the dynamics of the side force response to different mass flow rates applied to either the port or starboard actuator. Based on the linear time-invariant model, a proportional–integral control law was developed for set-point tracking a prescribed side force. The development of the linear time-invariant model, and corresponding linear time …
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