Blended control, predictor-corrector guidance algorithm: an enabling technology for Mars aerocapture.
A guidance scheme designed for coping with significant dispersion in the vehicle's state and atmospheric conditions is presented. In order to expand the flyable aerocapture envelope, control of the vehicle is realized through bank angle and angle-of-attack modulation. Thus, blended control of the vehicle is achieved, where the lateral and vertical motions of the vehicle are decoupled. The overall implementation approach is described, together with the guidance algorithm macrologic and structure. Results of guidance algorithm tests in the presence of various single and multiple off-nominal conditions are presented and discussed.
Jits
Roman Y
RY
NASA Ames Research Center, Moffett Field, CA 94035, USA.
Walberg
Gerald D
GD
D000465:Algorithms; D018480:Astronauts; D001272:Atmosphere; D003198:Computer Simulation; D004867:Equipment Design; D005118:Extraterrestrial Environment; D005240:Feasibility Studies; D006801:Humans; D018471:Hypergravity; D018535:Mars; D013026:Space Flight / Q000295:instrumentation*; D018531:Spacecraft; D014893:Weightlessness