Abstract
Aiming at the high precision requirement of the orbit determination system, an autonomous optical navigation strategy based on B-plane coordinate system was investigated for a small-body impact mission, in which the angle between the target-relative position and velocity vectors could be ignored. The algorithm used images of the target body to update target relative state information. This involved using the object center-of-figure data as the observations and then processing the data through a Kalman filter to update the impactor position and attitude components in the B-plane coordinate. Monte Carlo simulations demonstrate the feasibility of the approach, including the numerical accuracy and stability.
| Original language | English |
|---|---|
| Pages (from-to) | 1979-1982 |
| Number of pages | 4 |
| Journal | Xitong Fangzhen Xuebao / Journal of System Simulation |
| Volume | 21 |
| Issue number | 7 |
| State | Published - 5 Apr 2009 |
Keywords
- Attitude estimation
- Autonomous optical navigation
- Kalman filter
- Small body impact
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