By now, it must be obvious to the reader that the major goal for this book is to present various modern optimal control and adaptive guidance design techniques that are best suited in application to the satellite formation flying problems. Namely, the following design techniques have been discussed in detail in various preceding chapters: (i) Infinite-time linear quadratic regulator (LQR), (ii) Infinite-time state-dependent Riccati Equation (I-SDRE), (iii) Adaptive LQR, (iv) Adaptive dynamic inversion (DI) (v) Finite-time linear quadratic regulator (F-LQR), (vi) Finite-time state-dependent Riccati Equation (F-SDRE), and (vii) both discrete and continuous versions of model predictive static programming (MPSP). It is apparent, a curious reader would definitely want a comparative study to figure out the best performing method for the problem in hand. This chapter is aimed at to bring out the performance aspects of various methods presented in the earlier chapters.
Performance Comparison
Satellite Formation Flying ; Kapitel : 8 ; 139-146
2021-03-16
8 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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