NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Visual display aid for orbital maneuvering - Design considerationsThis paper describes the development of an interactive proximity operations planning system that allows on-site planning of fuel-efficient multiburn maneuvers in a potential multispacecraft environment. Although this display system most directly assists planning by providing visual feedback to aid visualization of the trajectories and constraints, its most significant features include: (1) the use of an 'inverse dynamics' algorithm that removes control nonlinearities facing the operator, and (2) a trajectory planning technique that separates, through a 'geometric spreadsheet', the normally coupled complex problems of planning orbital maneuvers and allows solution by an iterative sequence of simple independent actions. The visual feedback of trajectory shapes and operational constraints, provided by user-transparent and continuously active background computations, allows the operator to make fast, iterative design changes that rapidly converge to fuel-efficient solutions. The planning tool provides an example of operator-assisted optimization of nonlinear cost functions.
Document ID
19930039521
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Grunwald, Arthur J.
(Technion - Israel Inst. of Technology Haifa, United States)
Ellis, Stephen R.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 16, 2013
Publication Date
February 1, 1993
Publication Information
Publication: Journal of Guidance, Control, and Dynamics
Volume: 16
Issue: 1
ISSN: 0731-5090
Subject Category
Man/System Technology And Life Support
Accession Number
93A23518
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available