Title of article :
Incremental Predictive Command of Velocity to Be Gained Guidance Method
Author/Authors :
Ghahramani, N. amirkabir university of technology - Dept of Aerospace Eng, تهران, ايران , Naghash, A. amirkabir university of technology - Dept of Aerospace Eng, تهران, ايران , Towhidkhah, F. amirkabir university of technology - Dept of Biomedical Eng, تهران, ايران
From page :
99
To page :
105
Abstract :
In this paper, a new incremental predictive guidance method based on implicit form of velocity to be gained algorithm is proposed. In this approach, the generalized incremental predictive control (GIPC) approach is applied to the linearized model to compensate for the guidance error. Instead of using the present state in popular model based predictive controller (MPC), in the new method both previous and present states are utilized. GIPC approach introduces a feedback action including the weighted difference of the process states and the summation of the control action increments. To evaluate the robustness and performance of the proposed approach, the parameter uncertainties of the guidance and control are considered and a comparison with standard GPC is performed by extensive computer simulations. The results show a significant improvement in the robustness as well as tracking performance of the perturbed initial value of velocity to be gained or the reference signal.
Journal title :
Journal of Aerospace Science and Technology (JAST)
Journal title :
Journal of Aerospace Science and Technology (JAST)
Record number :
2747340
Link To Document :
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