Guidance method for detecting small-celestial-body-surface movement
A small celestial body and detector technology, applied in the field of aerospace, can solve problems such as poor control accuracy and uncertain influence of dynamic characteristics, and achieve the effect of improving robustness and control accuracy
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[0051] Step 1. Determine the initial velocity v i .
[0052] Use the three-axis ellipsoid model to construct small celestial bodies, the three semi-major axes are set to 3km, 2km and 1km respectively, and the density of the ellipsoid is 1200kg / m 3 , the spin angular velocity is 1.407×10 -4 rad / s.
[0053]Define R as the vector from the starting point [2181,309,669]m pointing to the single bounce target point [1763,0,809]m, then the unit vector in the R direction is:
[0054]
[0055] where R represents the modulus of the vector R. Define g as the gravitational acceleration vector at the starting point. In the R-g plane, let the vector l be perpendicular to R and point to the outside of the small celestial body. g l and g R are the components of the gravitational acceleration vector g along the l and R directions, respectively, and the expected bounce time t f Set to 1500s, then v i The velocity component along the l direction is:
[0056]
[0057] v i The velo...
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