Attitude control system for spacecraft with flexible appendages using H approach by Andra Venkateswarlu
Material type:![Book](/opac-tmpl/lib/famfamfam/BK.png)
- 629.4642 N96 "Thesis"
Item type | Current library | Call number | Status | Date due | Barcode |
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JRD Tata Memorial Library | 629.4642 N96 "Thesis" (Browse shelf(Opens below)) | Available | T03948 |
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