Deep space explorer acquisition phase celestial navigation method based on target object ephemeris correction
A technology for deep space probes and target celestial bodies is applied in the field of astronomical navigation in the capture segment of deep space probes based on target celestial ephemeris correction.
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[0091] The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments.
[0092] Such as figure 1 As shown, the target celestial bodies involved in the foregoing technical solutions can be celestial bodies in the solar system such as Mars, Venus, Jupiter, Saturn, etc., and Mars is used as an example below to illustrate the specific implementation process of the present invention:
[0093] 1. Establish a state model of deep space probes based on the gravitational orbital dynamics of the sun and eight planets
[0094] First initialize the position and velocity, set X=[xyzv x v y v z ] T is the state vector in the heliocentric inertial coordinate system, are the three-axis position and velocity of the detector in the heliocentric inertial coordinate system, X′=[x′y′z′v x 'v y 'v z '] T is the state vector in the center of fire inertial coordinate system, x′, y′, z′, v′ x , v′ y , v′ z are the three-axis po...
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