Abstract
Re-entry aircraft depends on aerodynamic force during flight. Because of windward rudder and lee rudder, there certainly exists aerodynamic coupling among pitch channel, yaw channel and roll channel under the situation of large attack angle and slip angle, and behaves couplings of inputs and states. This paper proposed decouple control of inputs aiming at the coupling problem of inputs, and the MIMO problem is transformed to a SISO one. For the SISO problem, the coupling of states can be solved by control system design to guarantee system stable and robust.
| Original language | English |
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| Title of host publication | Proceedings of 2012 International Conference on Modelling, Identification and Control, ICMIC 2012 |
| Pages | 534-537 |
| Number of pages | 4 |
| Publication status | Published - 2012 |
| Event | 2012 International Conference on Modelling, Identification and Control, ICMIC 2012 - Wuhan, China Duration: 24 Jun 2012 → 26 Jun 2012 |
Publication series
| Name | Proceedings of 2012 International Conference on Modelling, Identification and Control, ICMIC 2012 |
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Conference
| Conference | 2012 International Conference on Modelling, Identification and Control, ICMIC 2012 |
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| Country/Territory | China |
| City | Wuhan |
| Period | 24/06/12 → 26/06/12 |
Keywords
- attitude control
- decouple control of inputs
- re-entry maneuver warhead
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Ni, S., Shan, J., & Shang, S. (2012). Research of input decouple method of re-entry aircraft. In Proceedings of 2012 International Conference on Modelling, Identification and Control, ICMIC 2012 (pp. 534-537). Article 6260321 (Proceedings of 2012 International Conference on Modelling, Identification and Control, ICMIC 2012).