Volume 23 Issue 10
Oct.  2008
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SUN Chun-zhen, HUANG Yi-min, GUO Suo-feng. Reusable launch vehicle pitch attitude control system research by trajectory linearization[J]. Journal of Aerospace Power, 2008, 23(10): 1921-1926.
Citation: SUN Chun-zhen, HUANG Yi-min, GUO Suo-feng. Reusable launch vehicle pitch attitude control system research by trajectory linearization[J]. Journal of Aerospace Power, 2008, 23(10): 1921-1926.

Reusable launch vehicle pitch attitude control system research by trajectory linearization

  • Received Date: 2007-08-11
  • Rev Recd Date: 2008-04-29
  • Publish Date: 2008-10-28
  • To improve the performance of terminal area energy management control system for reusable launch vehicle,the pitch attitude control system architecture based on trajectory linearization was developed,which includes two parts: pseudo-inverse model and feedback control system.Using the concept of instantaneous equilibrium,the pseudo-inverse model was designed by trimming the whole profile and the pitch attitude control system architecture was built.Take example for the flight phase of high altitude and super sonic,the system was designed and compared with traditional feedback control system.The results show that the control system by trajectory linearization can improve the transition performance,offload the feedback loop,and reduce the possibility of integrator saturation.

     

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