Guidance of a spacecraft with low lift-to-drag ratio to a landing point.
- Published in:
- Cosmic Research, 2010, v. 48, n. 6, p. 534, doi. 10.1134/S0010952510060067
- By:
- Publication type:
- Article
Works matching DE "SPACE vehicle guidance systems"
Results: 7
1
2
Formulation of the problem of inertial navigation: A group theory approach.
- Published in:
- Cosmic Research, 2007, v. 45, n. 2, p. 176, doi. 10.1134/S0010952507020128
- By:
- Publication type:
- Article
3
Investigation of uav systems and flight modes for photogrammetric applications.
- Published in:
- Photogrammetric Record, 2011, v. 26, n. 136, p. 400, doi. 10.1111/j.1477-9730.2011.00657.x
- By:
- Publication type:
- Article
4
Coning Error Analysis and Compensation in Rotation Inertial Navigation System.
- Published in:
- Journal of Nanjing University of Aeronautics & Astronautics / Nanjing Hangkong Hangtian Daxue Xuebao, 2012, v. 44, n. 2, p. 159
- By:
- Publication type:
- Article
5
Electrodynamic control for spacecraft attitude stability in the geomagnetic field.
- Published in:
- Cosmic Research, 2014, v. 52, n. 6, p. 472, doi. 10.1134/S001095251406001X
- By:
- Publication type:
- Article
6
Methods and software for computer-aided design of the spacecraft guidance, navigation and control systems.
- Published in:
- Mathematics in Engineering, Science & Aerospace (MESA), 2016, v. 7, n. 4, p. 613
- By:
- Publication type:
- Article
7
Mathematical modeling of spacecraft guidance and control system in 3D space orbit transfer mission.
- Published in:
- Computational & Applied Mathematics, 2016, v. 35, n. 3, p. 865, doi. 10.1007/s40314-015-0290-8
- By:
- Publication type:
- Article