The DOI matches its Crossref record.
Quarternion feedback regulator for spacecraft eigenaxis rotations
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Research works printed but not linked: 31
- Junkins J. L, 1983, Journal of the Astronautical Sciences, 31, 217
- 10.2514/3.20096 · DOI
- 10.2514/3.55885 · DOI
- Cochran J. E., 1985, AIAA Paper
- 10.1016/0005-1098(86)90082-8 · DOI
- 10.2514/3.20173 · DOI
- Vadali S. R., 1984, Journal of the Astronautical Sciences, 32, 105
- 10.2514/3.20073 · DOI
- 10.2514/3.20095 · DOI
- 10.1080/0020718508961126 · DOI
- Mortensen R. E., 1963, Electronics Research Laboratory, Univ. of California
- 10.1080/00207176808905679 · DOI
- Meyer G., 1966, NASA TN D-36-43
- Hrastar J., 1970, NASA TN D-5959
- 10.2514/3.5598 · DOI
- 10.2514/3.19988 · DOI
- Brackenridge W. G., 1983, AAS/AIAA Paper
- 10.2514/3.20233 · DOI
- Robinson A. C., 1958, Wright Air Development Center, Wright-Patterson AFB, WADC Tech. Rept., 58, 21
- Margulies G., 1963, On Real Four-Parameter Representations of Satellite Attitude Motions
- 10.1115/1.3629605 · DOI
- 22 Whittaker, E. T., A Treatise on the Analytical Dynamics of Particles and Rigid Bodies, 4th ed.Dover, New York, 1937, pp.8-16.
- 10.2514/3.55830 · DOI
- 10.2514/3.56124 · DOI
- 10.2514/3.19831 · DOI
- 10.1115/1.3422907 · DOI
- 10.1115/1.3657268 · DOI
- Junkins J. L., 1981, American Astronautics Society Paper, 81
- 10.1115/1.3662604 · DOI
- LaSalle J., 1961, Stability by Lyapunov's Direct Method with Applications
- Bryson A. E., Jr., 1975, -C., Applied Optimal Control
Cited by
Sorted by citations
3CAT-2: Attitude Determination and Control System for a GNSS-R Earth Observation 6U CubeSat Mission
Cortiella, A., Vidal, D., Jané, J., Juan, E., Olivé, R., Amézaga, A., Munoz, J. F., Carreno-Luengo, P. V. H., & Camps, A. (2016) · European Journal of Remote Sensing · doi:10.5721/eujrs20164940 · Cited by 23
Attitude Trajectory Optimization for Agile Satellites in Autonomous Remote Sensing Constellations
Sin, E., Arcak, M., Nag, S., Ravindra, V., Li, A., & Levinson, R. (2021) · AIAA Scitech 2021 Forum · doi:10.2514/6.2021-1470 · Cited by 8
Metadata
- Authors
- Wie, B., Weiss, H., & Arapostathis, A.
- Affiliations
- The University of Texas at Austin (US)
- Venue
- Journal of Guidance, Control, and Dynamics
- Published
- 1989-05
- Volume
- 12
- Issue
- 3
- Pages
- 375-380
- ISSN
- 0731-5090 (ISSN-L)
- 1533-3884
- OpenAlex
- W1990181132
- Cited by
- 544
- References
- 0
- Citations by year
- 2026: 15 · 2025: 9 · 2024: 12 · 2023: 13 · 2022: 24 · 2021: 27 · 2020: 21 · 2019: 21 · 2018: 17 · 2017: 25 · 2016: 21 · 2015: 29 · 2014: 22 · 2013: 19 · 2012: 18
- FWCI
- 26.85
- Type
- journal article
- Language
- en
- Open access
- closed
- Locations
- Journal of Guidance Control and Dynamics (publishedVersion)
- Topics
- Physical Sciences › Engineering › Aerospace Engineering › Spacecraft Dynamics and Control
- Physical Sciences › Engineering › Aerospace Engineering › Guidance and Control Systems
- Physical Sciences › Engineering › Aerospace Engineering › Advanced Control and Stabilization in Aerospace Systems
- Keywords
- spacecraft attitude control, spacecraft rotation
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Registry, retraction, Cites and statistics results are computed, not judged, with one exception: a printed reference that no index lists is read once by a model before it counts as a citation error. Claims are extracted by a model and kept only when their quote appears verbatim in the text; each cited source is then checked, with a model’s help, for whether it says what the claim relies on. Those verdicts can be wrong — read the claim’s quote and the cited source before relying on one.
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