Системы навигации, наведения и управления полетом
Об этой коллекции
Данная коллекция документов была собрана Бобом Эндрепонтом [1] на сайте Geocities [2]. В составлении данной коллекции также участвовали Jim McDade, Reuben Barton, редакторы сайта «Apollo Lunar Surface Journal» [3], редакторы сайта «Apollo Flight Journal» [4], Кипом Теагу [5] и Марком Грейем [6].
Системы навигации, наведения и управления полетом
- Space Navigation Guidance and Control, Volume 1
- Space Navigation Guidance and Control, Volume 2
- Study of powered descent trajectories for manned lunar landings, Project Apollo, August 9, 1963
- NASA TM X-58040 Apollo Lunar Decent and Ascent Trajectories (ALSJ)
- Apollo CSM and LM onboard navigation system constraints
- Apollo: Guidance and control system
- Apollo: Guidance and control system 2
- NASA TND 6846 Apollo Experience Report-Mission Planning for Lunar Module Decent and Ascent pages 1-18 (ALSJ)
- NASA TND 6846 Apollo Experience Report-Mission Planning for Lunar Module Decent and Ascent pages 19-42 (ALSJ)
- APOLLO LUNAR-DESCENT GUIDANCE
- A LM powered descent strategy
- Possible Simplification of the Apollo Entry Guidance
- LM powered descent trajectory for the Apollo lunar landing mission
- LM Descent Guidance for a Feasibility Study to Simplify Apollo Guidance
- LM powered ascent trajectory for the Apollo lunar landing mission
- Project Apollo - A proposed LEM descent trajectory and fuel budget
- Simplified Software for the Apollo Guidance Computer - CSM Powered Flight Programs
- Apollo mission techniques. Mission C-prime lunar (alternate 1) translunar midcourse corrections and lunar orbit insertion. Volume 1: Techniques description, revision A
- Preliminary analysis of LM abort and CSM rescue from 60-n. mi. CSM orbit during the Hohmann descent phase
- Analysis of current LEM powered-descent trajectories
- Project Apollo. A preliminary simulation study of the required velocity meter sensitivity and touchdown control performance during lunar landing
- Apollo guidance and navigation. Volume 2 Primary G and N system lunar orbit operations
- Description of Apollo Entry Guidance
- MIT's role in Project Apollo. Volume 3: Computer subsystem
- MIT's role in Project Apollo. Volume 5: The software effort
- Apollo Lunar-Descent Guidance
- Reliability history of the Apollo guidance computer
- Lunar descent and ascent trajectories
- Delta V performance of the Apollo LM ascent trajectory
- Dynamic analysis of the LEM flight control system
- Apollo guidance and navigation. Guidance and navigation system for lunar excursion module (1962)
- Preliminary analysis of LM abort and CSM rescue from a 60-n mi. circular orbit following an LM abort from powered descent
- Manual abort guidance from the midcourse region of a lunar mission
- A linearized error analysis of onboard primary navigation systems for the Apollo lunar module
- A simplified guidance scheme for aborting lunar landings
- Analysis of sextant navigation measurements during lunar module rendezvous
- A simple abort scheme for lunar landings
- Revised LM descent and ascent delta V budgets for the lunar landing mission
- A method for star vector determination from alignment optical telescope sighting
- Real-time data processing and orbit determination on the Apollo tracking ships
- Apollo navigation ground and onboard capabilities
- Summary of Apollo guidance and navigation error analysis
- Maximum allowable lateral velocity errors during LM powered descent - Program Apollo
- Apollo Primary Guidance Navigation and Control System, addendum PGNCS Final report
page revision: 3, last edited: 28 Sep 2009 07:08
