Inertial navigation position error estimation, using vision system
The main task of the study is to estimate the position error in an inertial navigation system by integrating it with the visual system. The case study is a spacecraft that must accurately measure its position relative to a predetermined landing point. The spacecraft is assumed to be augmented GNSS n...
| Main Authors: | , |
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| Format: | Article |
| Language: | fas |
| Published: |
Aerospace Research Institute
2021-09-01
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| Series: | فصلنامه علوم و فناوری فضایی |
| Subjects: | |
| Online Access: | https://jsst.ias.ir/article_119299_973ac325413631488ef0d6ecc86aee01.pdf |