NOVOSELOV, 1972 - Google Patents
The problem of choosing a zero approximation of the angular position of an oriented satellite in the case of a nondipolar approximation of the geomagnetic fieldNOVOSELOV, 1972
- Document ID
- 3148426647572294876
- Author
- NOVOSELOV V
- Publication year
- Publication venue
- Mechanics of controlled motion and problems of cosmic dynamics.(A 73-31226 15-30) Leningrad, Izdatel'stvo Leningradskogo Universiteta, 1972,
External Links
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| NOVOSELOV | The problem of choosing a zero approximation of the angular position of an oriented satellite in the case of a nondipolar approximation of the geomagnetic field | |
| NOVOSELOV | Choice of a zero approximation of the angular position of a satellite on a trajectory segment of oriented motion in the case of a dipolar approximation of the geomagnetic field | |
| Stepanov | On the steady motions of a gyrostat satellite(Gyrostabilized satellite steady state motions in Newtonian force field having displaced satellite center of mass orbital plane relative to center of attraction) | |
| LAGASSE et al. | Synthesis of studies on the satellite stabilization by ion thrusters(Design of satellite telecommunication system stabilized by ion thrusters) | |
| KUMMER | General introduction to spacecraft attitude determination and related topics(Satellite attitude determination including stabilization methods and sensing systems) | |
| COPE | Attitude control for sun-pointing scientific satellites(Attitude control for sun-pointing scientific satellites, considering control loop, sun sensor and actuator control torques) | |
| Morozov | Stability of the relative equilibrium of a satellite under the action of gravitational, magnetic, and aerodynamic moments(Gyrostat satellite equilibrium positions in circular equatorial orbit under action of gravitational magnetic and aerodynamic moments based on gyrostabilized satellite equations of motion) | |
| BLATT | Orbital cryogenic acquisition and transfer(Low gravity propellant control, using capillary devices in large scale cryogenic vehicles) | |
| BERTIN et al. | Veronique v 27 sounding rocket attitude calculation using three magnetic sensors and taking into account continuity of movement and angular motion | |
| JONES | Neuter docking mechanism study(Neuter docking mechanisms for spacecraft) | |
| SUNESSON | Design of attitude loops for the L. A. S(Guidance sensor loops design for ESRO large astronomical satellite attitude control) | |
| SIMON et al. | The objectives and design of the inertial reference unit for the lunar orbiter(Lunar orbiter objectives, mission and spacecraft configuration, detailing inertial reference unit) | |
| CANNON | The vector reticle and control action display in manual control of space vehicle attitude(Manual three-axis satellite attitude control, using vector reticle and control action display concepts) | |
| POHER | The Cassiopeia system(Attitude control of sounding rockets by inertial and stellar sensor for stellar oriented experiments) | |
| KORENEV | The Mechanics of Guided Bodies(Book on mechanics of controlled body including control system realization, motion programming, dynamic error assessment and three-dimensional problems) | |
| Sergeev | Periodic solutions of the equations of motion of a heavy solid body around a fixed point(Periodic solutions for small nutation angle of quasi-linear autonomous system of equations of motion of heavy solid body moving around fixed point) | |
| LITVIN-SEDOI | The dynamics of a heavy gyroscope of variable size in the presence of rectilinear motion on the point of support(Variable size heavy gyroscope dynamics in presence of rectilinear motion on point of support) | |
| SOO | Use of reaction wheel tachometer feedback in the coarse attitude control loop of the L. A. S(Use of reaction wheel tachometer feedback in coarse attitude control loop of large astronomical satellite) | |
| SCHIEHLEN | Two different approaches for a control law of single gimbal control moment gyros(Gimbal angle and gimbal rate approaches for SGCMG control law) | |
| KONDURAR | On the presence of resonance phenomena in the motions of a satellite, resulting from its shape and the form of its orbit(Resonance effect of spheric inertia on vehicle rotating around spherical planet) | |
| OKHOTSIMSKII et al. | The motion of spacecraft in the atmosphere(Atmospheric reentry trajectory of space vehicle at orbital velocities and constant lift-drag ratio) | |
| DAMBECK | Geostationary satellite position and attitude determination using picture landmarks(Position and attitude determination for geostationary satellites from relative orientation of landmarks) | |
| MARTINIDES | The space environment- A survey(Earth orbiting satellite influence on satellite design with respect to acceleration, vibration and shocks, weightlessness, gas pressure, electromagnetic radiation, and magnetic fields) | |
| SILVERSTEIN | Implications of visual space perception theory for a long duration space mission | |
| TRACY | A satellite attitude control system using propane(Propane satellite control system with nitrogen control unit) |