Title of article
An adaptive predictor–corrector reentry guidance based on self-definition way-points
Author/Authors
Yong، نويسنده , , En-mi and Qian، نويسنده , , Wei-qi and He، نويسنده , , Kai-feng، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2014
Pages
11
From page
211
To page
221
Abstract
An adaptive predictor–corrector reentry guidance algorithm with self-defined way-points is proposed. In the guidance process, the reentry trajectory is divided into the predictor–corrector phase and the trajectory onboard generation and tracking phase which is near to the endpoint position of reentry and utilized to improve the accuracy and adaptivity of the guidance. In the first phase, the predictor–corrector algorithm is applied to solve the guidance problem between the self-defined way-points. Moreover the position parameters of reentry trajectory are translated into the parameters related to the reentry plane by orthogonal transformation in the spherical coordinate to improve robustness of guidance algorithm. In addition, the predictor–corrector algorithm is implemented using a brain emotional learning based intelligence controller (BELBIC). In the second phase, the trajectory from the current point to the endpoint is generated onboard and the linear–quadratic regulator (LQR) theory is employed for trajectory tracking. The effectivity of the proposed guidance is validated by simulations in conditions of the nominal case, the environment dispersed case and the endpoint maneuvering case. The advantages of this guidance in coping with disturbances, reducing time of numerical trajectory prediction and being suitable for maneuver endpoint are analyzed with the simulation results.
Keywords
Way-points , Predictor–corrector , BELBIC , Reentry , Guidance
Journal title
Aerospace Science and Technology
Serial Year
2014
Journal title
Aerospace Science and Technology
Record number
2231453
Link To Document