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The problem of orbit determination using one or two GPS satellites is discussed. Methods of getting initial values based on
linear translation is presented; the Secant method and the descend Newton iterative procedure and the continuation algorithm
are used synthetically to solve the nonlinear equations. Computer simulation shows that this algorithm can give preliminary
state of satellite orbit with a certain precision in short time. 相似文献
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Let q be a large prime, and χ the quadratic character modulo q. Let Φ be a self-dual Hecke-Maass cusp form for SL(3, Z), and uj a Hecke-Maass cusp form for Γ0(q) ? SL(2, Z) with spectral parameter tj. We prove, for the first time, some hybrid subconvexity bounds for the twisted L-functions on GL(3), such as L(1/2, Φ× uj ×χ) ?_(Φ,ε)(q(1 + |tj |))~(3/2-θ+ε) and L(1/2 + it, Φ×χ) ?_(Φ,ε)(q(1 + |t|))~(3/4-θ/2+ε) for any ε 0, where θ = 1/23 is admissible. The proofs depend on the first moment of a family of L-functions in short intervals. In order to bound this moment, we first use the approximate functional equations, the Kuznetsov formula, and the Voronoi formula to transform it to a complicated summation, and then we apply different methods to estimate it, which give us strong bounds in different aspects. We also use the stationary phase method and the large sieve inequalities. 相似文献
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We prove a non-vanishing result for central values of L-functions on GL(3), by using the mollification method and the Kuznetsov trace formula. 相似文献
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The Ramanujan Journal - In this note, we give a detailed proof of an asymptotic for averages of coefficients of a class of degree three L-functions which can be factorized as a product of a degree... 相似文献