How Changes in Patent Law May Affect Doctor Inventors

Abstract

All spacecraft attitude estimation methods are based on Wahbaʼs optimization problem. This problem can be reduced to finding the largest eigenvalue and the corresponding eigenvector for Davenportʼs K-matrix. Several iterative algorithms, such as QUEST and FOMA, were proposed, aiming at reducing the computational cost. But their computational time is unpredictable because the iteration number is not fixed and the solution is not accurate in theory. Recently, an analytical solution, ESOQ was suggested. The advantages of analytical solutions are that their computational time is fixed and the solution should be accurate in theory if there is no numerical error. In this paper, we propose a different analytical solution to Wahbaʼs problem. We use simple and easy to be verified examples to show that this method is numerically more stable than ESOQ, potentially faster than QUEST and FOMA. We also use extensive simulation test to support this claim.