AIAA Atmospheric Flight Mechanics Conference and Exhibit 2001
DOI: 10.2514/6.2001-4326
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A comparison of different guidance schemes for a direct fire rocket with a pulse jet control mechanism

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Cited by 15 publications
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“…The main disadvantage of this method is that a high thrust of the single thruster is required to realize the guidance process effectively. In [7], the trajectory tracking and proportional navigation were compared and it was concluded that the second one presents a poor performance in the vertical plane resulting from a trajectory curvature due to gravity. In [8], the modified linear theory was used successfully to reduce the munition dispersion significantly.…”
Section: Introductionmentioning
confidence: 99%
“…The main disadvantage of this method is that a high thrust of the single thruster is required to realize the guidance process effectively. In [7], the trajectory tracking and proportional navigation were compared and it was concluded that the second one presents a poor performance in the vertical plane resulting from a trajectory curvature due to gravity. In [8], the modified linear theory was used successfully to reduce the munition dispersion significantly.…”
Section: Introductionmentioning
confidence: 99%