International Journal of Aerospace Engineering / 2015 / Article / Fig 8

Research Article

Firing Control Optimization of Impulse Thrusters for Trajectory Correction Projectiles

Figure 8

Correction performance of the optimum firing control scheme.
(a) Total number of thrusters tired versus time
(b) Total attack angle versus time
(c) Horizontal impact point deviation versus time
(d) Longitudinal impact point deviation versus time
(e) Cross range versus range
(f) Attitude versus range

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