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Guidance and control /
| Clasificación: | Libro Electrónico |
|---|---|
| Autor Corporativo: | |
| Otros Autores: | , |
| Formato: | Electrónico Congresos, conferencias eBook |
| Idioma: | Inglés |
| Publicado: |
New York :
Academic Press,
1962.
|
| Colección: | Progress in astronautics and rocketry ;
v. 8. |
| Temas: | |
| Acceso en línea: | Texto completo |
Tabla de Contenidos:
- A. Ascent. Launch-on-Time Analysis for Space Missions ; Application of Pontryagin's Maximum Principle in Determining the Optimum Control of a Variable- Mass Vehicle ; Optimalizing Techniques for Injection Guidance
- B. Space Operations. Station Keeping of Satellites in Rendezvous Compatible Orbits ; Injection Guidance Accuracy as Applied to Lunar and Interplanetary Missions ; Techniques for Error Analysis of Trajectories ; Calculus of Perturbations Applied to Lunar Mission Analysis ; Precision Tracking of Space Vehicles
- C. Descent. Terminal Guidance System for Soft Lunar Landing ; Longitudinal Range Control for a Lifting Vehicle Entering a Planetary Atmosphere ; Automatic Re-Entry Guidance at Escape Velocity
- D. Inertial Navigation ; Application of Sideband Folding Techniques to the Navigation Satellite System ; Damping an Inertial Navigation System ; Multiple Inertial System Operation in Long Term Navigation; Fundamental Limitations on Inertial Measurements
- E. Inertial Components. The King Inertial Navigation Gyro ; Design Features of the G8 Two Degree of Freedom Floated Gyroscope ; Miniature Integrating Gyro Design ; Principles of the Electric Vacuum Gyroscope
- F. Optical Navigation ; Infrared Navigation Sensors for Space Vehicles ; Optical Doppler for Space Navigation ; Noise Consideration in Designing a Traveling Wave Tube Mixer for Optical Heterodyning
- G. Adaptive Systems ; Model Reference Adaptive Systems to Improve Reliability ; Path-Adaptive Mode for Guiding Space Flight Vehicles
- H. Attitude Control. Effects of Solar Radiation Pressure on Satellite Attitude Control ; Momentum Vector Considerations in Wheel-Jet Satellite Control System Design ; Limit Cycles in Reaction Jet Attitude Control Systems Subject to External Torques ; Attitude Control System Using Logically Controlled Pulses ; Generalized Two-Impulse Scheme for Reorienting a Spin Stabilized Vehicle.