发明名称 Descent trajectory monitoring method for e.g. civil aircraft, involves controlling aircraft speed on required speed to follow schedule by adjusting angle, when aircraft is not below altitude provided on trajectory and beyond threshold
摘要 <p>The method involves controlling speed of an aircraft (2) on the speed required for following a schedule by adjusting a rolling angle, when the aircraft is not below the altitude provided on a trajectory (1) and beyond an altitude threshold (S1). Engine thrust is adjusted, when the aircraft is below the altitude provided on the trajectory and above the threshold to control the speed of the aircraft. An independent claim is also included for a system for monitoring descent trajectory by an aircraft.</p>
申请公布号 FR2908532(A1) 申请公布日期 2008.05.16
申请号 FR20060009845 申请日期 2006.11.10
申请人 THALES SOCIETE ANONYME 发明人 DEKER GUY
分类号 G05D1/00;G08G5/04 主分类号 G05D1/00
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