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Space shuttle guidance, navigation, and control design equations. Volume 3: GuidanceSpace shuttle guidance, navigation, and control design equations are presented. The space-shuttle mission includes three relatively distinct guidance phases which are discussed; atmospheric boost, which is characterized by an adaptive guidance law; extra-atmospheric activities; and re-entry activities, where aerodynamic surfaces are the principal effectors. Guidance tasks include pre-maneuver targeting and powered flight guidance, where powered flight is defined to include the application of aerodynamic forces as well as thruster forces. A flow chart which follows guidance activities throughout the mission from the pre-launch phase through touchdown is presented. The main guidance programs and subroutines used in each phase of a typical rendezvous mission are listed. Detailed software requirements are also presented.
Document ID
19730023781
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Date Acquired
September 2, 2013
Publication Date
March 15, 1973
Subject Category
Navigation
Report/Patent Number
NASA-TM-X-69524
JSC-04217-REV-D-VOL-3
Accession Number
73N32514
Funding Number(s)
PROJECT: PROJ. SPACE SHUTTLE
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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