Haeussermann, 1965 - Google Patents
Guidance and control of Saturn launch vehiclesHaeussermann, 1965
- Document ID
- 3149108394926157935
- Author
- Haeussermann W
- Publication year
- Publication venue
- 2nd Annual Meeting
External Links
Snippet
The navigation, guidance, and control modes and problems of the Sam" launch vehicles are given as the requirements for the guidance and control method+. Two path adaptive guidance modes, featuring flight path optimization, in the form of a poL~ momis1 mode and …
- 230000010006 flight 0 abstract description 66
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
- B64G1/281—Spin-stabilised spacecraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/40—Arrangements or adaptations of propulsion systems
- B64G1/402—Propellant tanks; Feeding propellants
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
- G01C19/02—Rotary gyroscopes
- G01C19/34—Rotary gyroscopes for indicating a direction in the horizontal plane, e.g. directional gyroscopes
- G01C19/38—Rotary gyroscopes for indicating a direction in the horizontal plane, e.g. directional gyroscopes with north-seeking action by other than magnetic means, e.g. gyrocompasses using earth's rotation
Similar Documents
Publication | Publication Date | Title |
---|---|---|
LaCr | Application of nonlinear systems inverses to automatic flight control design-System concepts and flight evaluations | |
Beals et al. | Hubble Space Telescope precision pointing control system | |
Haeussermann | Guidance and control of Saturn launch vehicles | |
Haeussermann | Description and performance of the Saturn launch vehicle's navigation, guidance, and control system | |
Cannon Jr | Alignment of inertial guidance systems by gyrocompassing-linear theory | |
Gupta et al. | Development of navigation guidance and control technology for Indian launch vehicles | |
COCHRAN, JR et al. | Launcher/rocket dynamics and passive control | |
Palmer et al. | Analysis and simulation of a high accuracy spacecraft separation system. | |
Orr et al. | The Enduring Legacy of Saturn V Launch Vehicle Flight Dynamics and Control Design Principles and Practices | |
Angus et al. | The guidance system for Ariane | |
Lee | A digital flight control system design approach for a space shuttle booster type vehicle | |
HWANGBO et al. | Thermal design, analysis, and performance of a solid propellant spin system | |
Ames et al. | A study of personnel propulsion devices for use in the vicinity of the moon, volume I | |
James | First Steps Toward Space | |
Polites | A magnetic torquing system for emergency stabilization and backup control of the LST | |
JAYARAMAN et al. | Nutation and precession control of the High Energy Solar Physics (HESP) satellite | |
Pue et al. | Configuration tradeoffs for the space infrared telescope facility pointing control system | |
Jackson et al. | Software validation of the Titan IIIC digital flight control system utilizing a hybrid computer | |
White | Investigation of the Errors of an Internal Guidance System During Satellite Re-entry | |
Hamilton | The staging dynamics of a proposed space shuttle configuration | |
Joshi | Analysis of a magnetically suspended, high-performance instrument pointing system | |
BERKE | Master reference system for rapid at sea alignment of aircraft inertial navigation systems | |
Grantham et al. | A system for inertial experiment pointing and attitude control | |
Draper et al. | GUIDANCE AND NAVl | |
Gordan | Centaur D1-A systems in a nutshell |