Robust roll modulation guidance for aeroassisted mars mission

Details Robust roll modulation guidance for aeroassisted mars mission Robust roll modulation guidance for aeroassisted mars mission

Mar 1995

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1995jgcd...18..298t&link_type=abstract

Journal of Guidance, Control, and Dynamics (ISSN 0731-5090), vol. 18, no. 2, p. 298-305

Computer Science

Performance

Aeroassist, Lateral Control, Maneuverability, Mars Probes, Spacecraft Guidance, Spacecraft Performance, Acceleration (Physics), Atmospheric Models, Computerized Simulation, Drag, Interplanetary Flight, Lift, Robustness (Mathematics)

Scientific paper

The utility of using an aggregate measure of a vehicle's performance in determining the gains in a fixed-structure guidance scheme for an aeromaneuvering spacecraft so as to increase the 'robustness' of the vehicle's performance is examined. The gains in the guidance scheme are determined by minimizing an 'averaged' performance measure based upon the vehicle's flight through several different atmosphere models. This technique is applied to a Martian aeromaneuvering problem. Simulation results using gains determined by this method show a significant increase in off-nominal performance.

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