Simplified Interplanetary Guidance Procedures Using Onboard Optical Measurements PDF Download
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Author | : Harold A. Hamer |
Publisher | : |
Total Pages | : 36 |
Release | : 1972 |
Genre | : Space trajectories |
ISBN | : |
Download Simplified Interplanetary Guidance Procedures Using Onboard Optical Measurements Book in PDF, ePub and Kindle
Author | : Harold A. Hamer |
Publisher | : |
Total Pages | : 0 |
Release | : 1971 |
Genre | : |
ISBN | : |
Download Simplified Interplanetary Guidance Using Onboard Optical Measurements Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 418 |
Release | : 1972 |
Genre | : |
ISBN | : |
Download NASA Technical Note Book in PDF, ePub and Kindle
Author | : Harold A. Hamer |
Publisher | : |
Total Pages | : 68 |
Release | : 1971 |
Genre | : Inertial navigation (Aeronautics) |
ISBN | : |
Download Midcourse and Approach Guidance Requirements for Simplified Onboard Control of Moon-to-earth Trajectories Book in PDF, ePub and Kindle
Author | : Harold A. Hamer |
Publisher | : |
Total Pages | : 50 |
Release | : 1971 |
Genre | : Optical measurements |
ISBN | : |
Download Fixed-angle Translunar Guidance Procedures Using Onboard Optical Measurements Book in PDF, ePub and Kindle
Onboard procedures requiring only simple calculations have been developed for midcourse and approach guidance for translunar trajectories. For midcourse guidance the procedure relies solely on an optical range measurement. The approach-guidance procedure requires a star-to-body measurement and may require a range measurement, depending on the distance to the moon. For both procedures the velocity-correction vector is applied in a fixed inertial direction. In the approach-guidance procedure either one or two guidance maneuvers are applied, depending on the accuracy desired and tile distance to the moon. An error analysis showed that perilune radius can be controlled to a onesigma accuracy of about 30 km.
Author | : Harold A. Hamer |
Publisher | : |
Total Pages | : 92 |
Release | : 1970 |
Genre | : Approach guidance |
ISBN | : |
Download An Approach Guidance Method Using a Single Onboard Optical Measurement Book in PDF, ePub and Kindle
An empirical method has been developed for onboard guidance within the sphere of influence of a celestial body. For guidance maneuvers made at a relatively large distance from the body, only one preselected measurement from a star to the body is required. Although the method is designed to control the magnitude of the periapsis radius (or entry angle), the periapsis position and velocity automatically remain close to the nominal values. For lunar approach, error analysis with an assumed one-sigma error of 10 seconds of arc in the optical angular measurements and a one-sigma velocity-cutoff error of 0.2 m/sec has shown that perilune radius can be controlled to a one-sigma accuracy of from 7 to 13 km, depending on the time the approach guidance is performed.
Author | : Harold A. Hamer |
Publisher | : |
Total Pages | : 90 |
Release | : 1967 |
Genre | : Navigation (Astronautics) |
ISBN | : |
Download Midcourse-guidance Procedure with Single Position Fix Obtained from Onboard Optical Measurements Book in PDF, ePub and Kindle
Author | : L. Keith Barker |
Publisher | : |
Total Pages | : 28 |
Release | : 1970 |
Genre | : Moon |
ISBN | : |
Download Simple Method of Using Onboard Optical Measurements to Predict the Orbit Established After the Lunar-ascent-transfer Orbit Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 400 |
Release | : 1995 |
Genre | : Aeronautics |
ISBN | : |
Download Scientific and Technical Aerospace Reports Book in PDF, ePub and Kindle
Author | : Harold A. Hamer |
Publisher | : |
Total Pages | : 40 |
Release | : 1971 |
Genre | : Optical measurements |
ISBN | : |
Download Fixed-angle Translunar Guidance Procedures Using Onboard Optical Measurements Book in PDF, ePub and Kindle
Onboard procedures requiring only simple calculations have been developed for midcourse and approach guidance for translunar trajectories. For midcourse guidance the procedure relies solely on an optical range measurement. The approach-guidance procedure requires a star-to-body measurement and may require a range measurement, depending on the distance to the moon. For both procedures the velocity-correction vector is applied in a fixed inertial direction. In the approach-guidance procedure either one or two guidance maneuvers are applied, depending on the accuracy desired and tile distance to the moon. An error analysis showed that perilune radius can be controlled to a onesigma accuracy of about 30 km.