Author: C. Dewey Havill
Publisher:
ISBN:
Category : Artificial satellites
Languages : en
Pages : 40
Book Description
An Emergency Midcourse Navigation Procedure for a Space Vehicle Returning from the Moon
Author: C. Dewey Havill
Publisher:
ISBN:
Category : Artificial satellites
Languages : en
Pages : 40
Book Description
Publisher:
ISBN:
Category : Artificial satellites
Languages : en
Pages : 40
Book Description
NASA Technical Note
Scientific and Technical Aerospace Reports
NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 262
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 262
Book Description
Midcourse and Approach Guidance Requirements for Simplified Onboard Control of Moon-to-earth Trajectories
Author: Harold A. Hamer
Publisher:
ISBN:
Category : Inertial navigation (Aeronautics)
Languages : en
Pages : 68
Book Description
Publisher:
ISBN:
Category : Inertial navigation (Aeronautics)
Languages : en
Pages : 68
Book Description
Monthly Catalog of United States Government Publications
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1304
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1304
Book Description
On-board Calculations of a Two-impulse Abort to a Preselected Landing Site
Author: Robert B. Merrick
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 36
Book Description
Preliminary Determination of Spacecraft Trajectories Using On-board Optical Measurements
Author: John D. McLean
Publisher:
ISBN:
Category : Optical measurements
Languages : en
Pages : 100
Book Description
This report cicals with the problcm of determining the trajectory of a spacecraft from on-board optical measurents without a priori information. Only sufficient information to determine the trajectory is used, and it is assumed that this preliminary estimate will be improved later by the use of differential corrections and redundant data. Five basic types of measurements, representing instruments considered feasible or within the state of the art, are considered. The effects of random and bias type measurement errors and interpolation errors arising from nonsimultaneous measurements are analyzed. Only observations of the central body and two stars are considered. Within certain limitations all five types of measurements will give satisfactory results. Two important factors discussed in the report are the proper choice of stars and the calibration for eliminating bias errors.
Publisher:
ISBN:
Category : Optical measurements
Languages : en
Pages : 100
Book Description
This report cicals with the problcm of determining the trajectory of a spacecraft from on-board optical measurents without a priori information. Only sufficient information to determine the trajectory is used, and it is assumed that this preliminary estimate will be improved later by the use of differential corrections and redundant data. Five basic types of measurements, representing instruments considered feasible or within the state of the art, are considered. The effects of random and bias type measurement errors and interpolation errors arising from nonsimultaneous measurements are analyzed. Only observations of the central body and two stars are considered. Within certain limitations all five types of measurements will give satisfactory results. Two important factors discussed in the report are the proper choice of stars and the calibration for eliminating bias errors.