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机译:使用火星网络实时导航火星任务
a: clock acceleration or oscillator aging, s/s2; a_A: acceleration measurement model of spacecraft acceleration in the accelerometer frame, m/s~2 a_A~B: true spacecraft acceleration vector in the body frame, m/s~2 a_(cg,ng,mod)~I: spacecraft acceleration because of modeled nongravitational forces in the inertial frame, m/s~2; B_R: bit rate, bps; B_w: filter bandwidth, Hz; b: clock bias, s; b_A: vector of accelerometer biases per axis, m/s~2; b_G: vector of gyro biases per axis, rad/s; C/N_0: carner power-to-noise density ratio; c(t): clock time, cycles; d: clock drift, s/s; E_b/N_0: bit energy-to-noise density ratio; e_r: unit vector in the direction of the vector r; F_(ng,dyn)~I: nongravitational forces acting on spacecraft center of gravity, N;
机译:ESA的火星探索计划:ExoMars任务和国际火星样本返回任务的准备活动
机译:火星-phobos:具有火星-月亮协同效应的火星任务架构
机译:Amadee-18:基于视觉的模拟火星任务的无人驾驶飞行器导航(AVI-NAV)
机译:2009年火星科学实验室的任务与导航设计。
机译:使用火星网络对火星最终方法进行实时导航。
机译:在模拟火星任务期间长期禁闭和运动对策对肌肉力量的影响:来自Mars500研究的数据
机译:火星网络辅助的实时火星进近导航
机译:火星网络辅助实时火星进近导航