Chinese Space Science and Technology ›› 2016, Vol. 36 ›› Issue (4): 17-.doi: 10.16708/j.cnki.1000-758X.2016.0042
Previous Articles Next Articles
KONG Xiang-Long, LI Wen-Long, LI Wen-Feng, ZHAO Yi
Received:
Revision received:
Online:
Published:
Abstract: Mostalgorithmsofinertiaparametersidentificationassumedthesystemmomentumknownandfewattentionwaspaidtotheattitudestabilizationofbase.Anincrementalformoftheidentificationequationwasgivenbasedontheconservationprincipleofmomentumandafractionalstepmethodwasproposed.Firstly,estimationequationsaboutthemassandpositionofmasscenterwereobtainedandtheunknownconstantlinearmomentumwaseliminatedinincrementalformulation.Theestimateoflinearmomentumwascalculatedwiththeestimatedparametersandthensubstitutedintoestimationequationsabouttheinertiatensors.Theincrementalequationswereobtainedagaintoeliminatetheunknownconstantangularmomentum.Anadaptivereactionlesscontrollerwasusedtopersistentlyexcitetherobotarm,whichguaranteedtheconvergenceofthealgorithmaswellasthestabilizationofbaseattitude.Simulationsresultsshowthatinertialparametersareaccuratelyidentifiedandtheangularvelocitiesofthebasearelessthan10-3,whichcanbeviewedasnearlyundisturbed.
Key words: uncooperativetarget, attitudestabilization, redundantdegreeoffreedom, inertiaparameteridentification, reactionnullspace, adaptivecontrol
KONG Xiang-Long, LI Wen-Long, LI Wen-Feng, ZHAO Yi. Inertiaparameteridentificationofonorbituncooperativeobject[J]. Chinese Space Science and Technology, 2016, 36(4): 17-.
Add to citation manager EndNote|Reference Manager|ProCite|BibTeX|RefWorks
URL: https://journal26.magtechjournal.com/kjkxjs/EN/10.16708/j.cnki.1000-758X.2016.0042
https://journal26.magtechjournal.com/kjkxjs/EN/Y2016/V36/I4/17