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 :
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