Robust Spacecraft Angular-Rate Estimation from Vector Observations Using Fast Interlaced Particle Filtering
- Author(s):
- Carmi, A. ( Technion - Israel Institute of Technology, Haifa, Israel )
- Oshman, Y.
- Publication title:
- AIAA meeting papers on disc
- Title of ser.:
- AIAA Paper : AIAA Guidance Navigation and Control Conference
- Ser. no.:
- 2005
- Pub. Year:
- 2005
- No.:
- 2005-6399
- Paper no.:
- AIAA Paper 2005-6399
- Pub. info.:
- [Reston, Va.]: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- Language:
- English
- Call no.:
- A07400/200516 [CD-ROM 2005 Disc 16]
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
Vector Observations-Based Gyroless Spacecraft Attitude/Angular Rate Estimation Using Particle Filtering
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
2
Technical Paper
Estimating Attitude from Vector Observations Using a Genetic Algorithm-Embedded Quaternion Particle Filter
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
3
Technical Paper
Fast Estimation of Spacecraft Angular Velocity from Sequential Geomagnetic Field Observations
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
12
Technical Paper
Sequential gyroless attitude/attitude-rate estimation using integrated-rate parameters
American Institute of Aeronautics and Astronautics |