Mars ascent-stage design utilizing nuclear propulsion
- 期刊名称Journal of Spacecraft and Rockets
- 作者Donahue, Benjamin B.
- 卷第32卷
- 期第3期
- 印刷ISSN0022-4650
- 电子ISSN1533-6794
- 文件大小1076.21KB
- 发表时间1995-05
- DOI10.2514/3.26650
- 页码552-558
Shaped Torque TechniquesSwigert, C.J. · Journal of Guidance, Control, and Dynamics · 1980
Multibody Model of an OrnithopterGrauer, Jared A.; Hubbard, James E. · Journal of Guidance, Control, and Dynamics · 2009
Predictive Missile GuidanceBest, R. A.; Norton, J. P. · Journal of Guidance, Control, and Dynamics · 2000
Optimal Deorbit GuidanceBaldwin, Morgan C.; Lu, Ping · Journal of Guidance, Control, and Dynamics · 2012
Adaptive Radome Compensation Using DitherZarchan, Paul; Gratt, Harvey · Journal of Guidance, Control, and Dynamics · 1999
Nonlinear Synergetic Optimal ControllersNusawardhana, Antonius; Zak, S. H.; Crossley, W. A. · Journal of Guidance, Control, and Dynamics · 2007
Symmetric Missile Dynamic InstabilitiesMurphy, Charles H. · Journal of Guidance, Control, and Dynamics · 1981
Missile and spacecraft coning instabilitiesPlatus, D. H. · Journal of Guidance, Control, and Dynamics · 1994