Mahajan, Bharat; Alfriend, Kyle T. Correction to: “Analytic orbit theory with any arbitrary spherical harmonic as the dominant perturbation”. (English) Zbl 1472.70048 Celest. Mech. Dyn. Astron. 133, No. 6, Paper No. 25, 3 p. (2021). MSC: 70M20 70H09 70F15 PDFBibTeX XMLCite \textit{B. Mahajan} and \textit{K. T. Alfriend}, Celest. Mech. Dyn. Astron. 133, No. 6, Paper No. 25, 3 p. (2021; Zbl 1472.70048) Full Text: DOI
Aristoff, Jeffrey M.; Horwood, Joshua T.; Alfriend, Kyle T. On a set of \(J_2\) equinoctial orbital elements and their use for uncertainty propagation. (English) Zbl 1466.70027 Celest. Mech. Dyn. Astron. 133, No. 3, Paper No. 9, 19 p. (2021). MSC: 70M20 PDFBibTeX XMLCite \textit{J. M. Aristoff} et al., Celest. Mech. Dyn. Astron. 133, No. 3, Paper No. 9, 19 p. (2021; Zbl 1466.70027) Full Text: DOI
Mahajan, Bharat; Alfriend, Kyle T. Analytic orbit theory with any arbitrary spherical harmonic as the dominant perturbation. (English) Zbl 1451.70048 Celest. Mech. Dyn. Astron. 131, No. 10, Paper No. 45, 25 p. (2019); correction ibid. 133, No. 6, Paper No. 25, 3 p. (2021). MSC: 70M20 70H09 70F15 PDFBibTeX XMLCite \textit{B. Mahajan} and \textit{K. T. Alfriend}, Celest. Mech. Dyn. Astron. 131, No. 10, Paper No. 45, 25 p. (2019; Zbl 1451.70048) Full Text: DOI
Mahajan, Bharat; Vadali, Srinivas R.; Alfriend, Kyle T. Exact Delaunay normalization of the perturbed Keplerian Hamiltonian with tesseral harmonics. (English) Zbl 1390.70061 Celest. Mech. Dyn. Astron. 130, No. 3, Paper No. 25, 25 p. (2018). MSC: 70M20 PDFBibTeX XMLCite \textit{B. Mahajan} et al., Celest. Mech. Dyn. Astron. 130, No. 3, Paper No. 25, 25 p. (2018; Zbl 1390.70061) Full Text: DOI
Weisman, R. M.; Majji, M.; Alfriend, K. T. Analytic characterization of measurement uncertainty and initial orbit determination on orbital element representations. (English) Zbl 1293.70075 Celest. Mech. Dyn. Astron. 118, No. 2, 165-195 (2014). MSC: 70M20 PDFBibTeX XMLCite \textit{R. M. Weisman} et al., Celest. Mech. Dyn. Astron. 118, No. 2, 165--195 (2014; Zbl 1293.70075) Full Text: DOI
Sengupta, Prasenjit; Vadali, Srinivas R.; Alfriend, Kyle T. Second-order state transition for relative motion near perturbed, elliptic orbits. (English) Zbl 1162.70023 Celest. Mech. Dyn. Astron. 97, No. 2, 101-129 (2007). MSC: 70M20 70F15 PDFBibTeX XMLCite \textit{P. Sengupta} et al., Celest. Mech. Dyn. Astron. 97, No. 2, 101--129 (2007; Zbl 1162.70023) Full Text: DOI
Gim, Dong-Woo; Alfriend, Kyle T. Satellite relative motion using differential equinoctial elements. (English) Zbl 1129.70331 Celest. Mech. Dyn. Astron. 92, No. 4, 295-336 (2005). MSC: 70M20 70F15 PDFBibTeX XMLCite \textit{D.-W. Gim} and \textit{K. T. Alfriend}, Celest. Mech. Dyn. Astron. 92, No. 4, 295--336 (2005; Zbl 1129.70331) Full Text: DOI
Vadali, S. R.; Vaddi, S. S.; Alfriend, K. T. An intelligent control concept for formation flying satellites. (English) Zbl 1098.70542 Int. J. Robust Nonlinear Control 12, No. 2-3, 97-115 (2002). MSC: 70M20 70Q05 93C85 PDFBibTeX XMLCite \textit{S. R. Vadali} et al., Int. J. Robust Nonlinear Control 12, No. 2--3, 97--115 (2002; Zbl 1098.70542) Full Text: DOI
Alfriend, Kyle T.; Vadali, Srinivas R.; Schaub, Hanspeter Formation flying satellites: Control by an astrodynamicist. (English) Zbl 0997.70023 Celest. Mech. Dyn. Astron. 81, No. 1-2, 57-62 (2001). Reviewer: Yoshihide Kozai (Suginami Tokyo) MSC: 70M20 70Q05 PDFBibTeX XMLCite \textit{K. T. Alfriend} et al., Celest. Mech. Dyn. Astron. 81, No. 1--2, 57--62 (2001; Zbl 0997.70023) Full Text: DOI
Schaub, Hanspeter; Alfriend, Kyle T. \(J_2\) invariant relative orbits for spacecraft formations. (English) Zbl 0989.70018 Celest. Mech. Dyn. Astron. 79, No. 2, 77-95 (2001). Reviewer: Yoshihide Kozai (Suginami Tokyo) MSC: 70M20 PDFBibTeX XMLCite \textit{H. Schaub} and \textit{K. T. Alfriend}, Celest. Mech. Dyn. Astron. 79, No. 2, 77--95 (2001; Zbl 0989.70018) Full Text: DOI
Alfriend, K. T.; Coffey, S. L. Elimination of the perigee in the satellite problem. (English) Zbl 0542.70033 Celestial Mech. 32, 163-172 (1984). MSC: 70M20 PDFBibTeX XMLCite \textit{K. T. Alfriend} and \textit{S. L. Coffey}, Celest. Mech. 32, 163--172 (1984; Zbl 0542.70033) Full Text: DOI
Coffey, S. L.; Alfriend, K. T. Satellite orbit theories based on the elimination of the parallax. (English) Zbl 0534.70026 The motion of planets and natural and artificial satellites, Proc. Symp., Embu/Braz. 1981, Math. Dyn. Astron. Ser. 2, 117-126 (1983). MSC: 70M20 85A99 PDFBibTeX XML
Longman, R. W.; Alfriend, K. T. Actuator placement from degree of controllability criteria for regular slewing of flexible spacecraft. (English) Zbl 0468.70030 Acta Astronaut. 8, 703-718 (1981). MSC: 70M20 85A99 93B05 93B40 PDFBibTeX XMLCite \textit{R. W. Longman} and \textit{K. T. Alfriend}, Acta Astronaut. 8, 703--718 (1981; Zbl 0468.70030) Full Text: DOI
Alfriend, K. T.; Dasenbrock, R.; Pickard, H.; Deprit, A. The extended phase space formulation of the Vinti problem. (English) Zbl 0384.70039 Celestial Mech. 16, 441-458 (1977). MSC: 70M20 70-04 70H20 70J99 PDFBibTeX XMLCite \textit{K. T. Alfriend} et al., Celest. Mech. 16, 441--458 (1977; Zbl 0384.70039) Full Text: DOI
Alfriend, Kyle T. Magnetic attitude control system for dual-spin satellites. (English) Zbl 0321.70011 AIAA J. 13, 817-822 (1975). MSC: 70M20 93C15 PDFBibTeX XMLCite \textit{K. T. Alfriend}, AIAA J. 13, 817--822 (1975; Zbl 0321.70011) Full Text: DOI
Alfriend, K. T.; Velez, C. E. The application of general perturbation theories to the artificial satellite problem. (English) Zbl 0316.70024 Acta Astronaut. 2, 577-591 (1975). MSC: 70M20 70F15 PDFBibTeX XMLCite \textit{K. T. Alfriend} and \textit{C. E. Velez}, Acta Astronaut. 2, 577--591 (1975; Zbl 0316.70024) Full Text: DOI