发明名称 AIRCRAFT FLIGHT MANAGEMENT SYSTEM
摘要 <p>A method comprising a first step of determining the point on the flightpath wherefrom it is theoretically no longer possible to comply with the required time constraint by following a pre-established speed profile, and a second step of computing a speed change and determining a fresh speed profile obtained by determining segment-by-segment speed corrections from said point up to the last modifiable segment. The speed change in each segment is restricted to a maximum value and the new speed is computed on the basis of the curve showing the flight time t as a function of the speed V, said curve being converged upon by a curve corresponding to the following equation having three coefficients (c1, c2, c3): V = c1 / t + c2 / t2 + c3 / t3. Compliance with time constraints may thus be ensured while meeting the requirements of the pilot and air traffic controllers.</p>
申请公布号 WO1997048028(A1) 申请公布日期 1997.12.18
申请号 FR1997001077 申请日期 1997.06.13
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