DocumentCode
25225
Title
Reachability Using Arbitrary Performance Indices
Author
Holzinger, Marcus J. ; Scheeres, Daniel J. ; Hauser, John
Author_Institution
Georgia Inst. of Technol., Atlanta, GA, USA
Volume
60
Issue
4
fYear
2015
fDate
Apr-15
Firstpage
1099
Lastpage
1103
Abstract
The problem of optimal reachability set computation with alternate performance indices and independent parameters for smooth value functions is motivated and examined. A General Independent Parameter Hamilton Jacobi Bellman PDE formulation is derived and an independent parameter mapping function is defined. Performance index metric properties are leveraged to define Generalized Metric Range Sets. For Newtonian systems it is shown that singular independent parameter mappings can be circumvented using constants of motion. Finally, the motivating problem is solved using the central results of this technical note to generate free-time, Δν-constrained orbital metric range sets.
Keywords
aerospace control; fuel; optimal control; partial differential equations; performance index; reachability analysis; Newtonian systems; alternate performance indices; arbitrary performance indices; fuel-optimal control; general independent parameter Hamilton Jacobi Bellman PDE formulation; generalized metric range sets; independent parameter mapping function; independent parameter mappings; motion constant; optimal reachability set computation; orbital metric range sets; performance index metric properties; smooth value functions; spacecraft; Dynamics; Fuels; Measurement; Optimal control; Optimized production technology; Space vehicles; Trajectory; Hamilton Jacobi Bellman partial differential equation (HJB PDE); Range; Reachability;
fLanguage
English
Journal_Title
Automatic Control, IEEE Transactions on
Publisher
ieee
ISSN
0018-9286
Type
jour
DOI
10.1109/TAC.2015.2391451
Filename
7014247
Link To Document