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    • 3. 发明授权
    • Systems and methods for RTA control of multi-segment flight plans with smooth transitions
    • 用于具有平滑过渡的多段飞行计划的RTA控制的系统和方法
    • US08406939B2
    • 2013-03-26
    • US12875371
    • 2010-09-03
    • Mike JacksonMichal PolanskyErwan ParicaudJiri Svoboda
    • Mike JacksonMichal PolanskyErwan ParicaudJiri Svoboda
    • G06F7/00
    • G05D1/101G08G5/0039G08G5/0052
    • Methods, systems and device are provided for smoothing a required time of arrival (RTA) speed transition for an aircraft in a multi-segmented speed profile including at least one preceding region with a first predetermined speed pad and at a speed constrained region with a second predetermined speed pad. Exemplary methods include, but are not limited to determining whether a speed constrained region is engaged by a preceding region based at least in part on a speed of an aircraft. If the speed constrained region is engaged, the instructions determine a revised second speed pad for the speed constrained region. If the speed constrained region is not engaged then the instructions assign a default speed pad as the second speed pad for the speed constrained region. The instructions also compile a new speed profile that is defined by one of the revised second speed pad and the default speed pad for the speed constrained region and transmit commands that accelerate the aircraft to a new speed based on the new speed profile.
    • 提供了方法,系统和装置,用于平滑用于具有第一预定速度垫的包括至少一个先前区域的多分段速度曲线中的飞行器的所需到达时间(RTA)速度转换,并且在速度约束区域处平滑第二 预定速度垫。 示例性方法包括但不限于至少部分地基于飞行器的速度来确定速度约束区域是否由前一区域接合。 如果速度约束区域被接合,则指令确定用于速度约束区域的经修改的第二速度焊盘。 如果速度约束区域未被接合,则指令将默认速度焊盘分配为用于速度约束区域的第二速度焊盘。 指令还编译一个新的速度曲线,由速度约束区域的修正后的第二速度挡块和默认速度盘之一定义,并且基于新的速度曲线将飞行器加速到新的速度。
    • 4. 发明申请
    • SYSTEMS AND METHODS FOR RTA CONTROL OF MULTI-SEGMENT FLIGHT PLANS WITH SMOOTH TRANSITIONS
    • 用于具有平滑过渡的多分段飞行计划的RTA控制的系统和方法
    • US20120059535A1
    • 2012-03-08
    • US12875371
    • 2010-09-03
    • Mike JacksonMichal PolanskyErwan ParicaudJiri Svoboda
    • Mike JacksonMichal PolanskyErwan ParicaudJiri Svoboda
    • G06F7/00
    • G05D1/101G08G5/0039G08G5/0052
    • Methods, systems and device are provided for smoothing a required time of arrival (RTA) speed transition for an aircraft in a multi-segmented speed profile including at least one preceding region with a first predetermined speed pad and at a speed constrained region with a second predetermined speed pad. Exemplary methods include, but are not limited to determining whether a speed constrained region is engaged by a preceding region based at least in part on a speed of an aircraft. If the speed constrained region is engaged, the instructions determine a revised second speed pad for the speed constrained region. If the speed constrained region is not engaged then the instructions assign a default speed pad as the second speed pad for the speed constrained region. The instructions also compile a new speed profile that is defined by one of the revised second speed pad and the default speed pad for the speed constrained region and transmit commands that accelerate the aircraft to a new speed based on the new speed profile.
    • 提供了方法,系统和装置,用于平滑用于具有第一预定速度垫的包括至少一个先前区域的多分段速度曲线中的飞行器的所需到达时间(RTA)速度转换,并且在速度约束区域处平滑第二 预定速度垫。 示例性方法包括但不限于至少部分地基于飞行器的速度来确定速度约束区域是否由前一区域接合。 如果速度约束区域被接合,则指令确定用于速度约束区域的经修改的第二速度焊盘。 如果速度约束区域未被接合,则指令将默认速度焊盘分配为用于速度约束区域的第二速度焊盘。 指令还编译一个新的速度曲线,由速度约束区域的修正后的第二速度挡块和默认速度盘之一定义,并且基于新的速度曲线将飞行器加速到新的速度。
    • 6. 发明授权
    • Resin composition for a sheet molding compound and method therefor
    • 用于片状模塑料的树脂组合物及其方法
    • US07317049B2
    • 2008-01-08
    • US10241826
    • 2002-09-10
    • John M. MaxelMike Jackson
    • John M. MaxelMike Jackson
    • C08K5/098C08K3/22
    • B29C70/502B29C70/18C08K5/0008
    • A sheet molding compound used for the preparation of enclosures comprising a base resin in a range from 20.0 to 28.0% by weight; a thermoplastic resin in a range from 3.0 to 7.0% by weight; a styrene monomer in a range from 0.01 to 2.5% by weight; a first catalyst in a range from 0.1 to 0.7% by weight; a second catalyst in a range from 0.01 to 0.3 % by weight; a catalyst modifier in a range from 0.01 to 0.25% by weight; an inhibitor in a range from 0.01 to 0.25% by weight; a UV absorber in a range from 0.01 to 0.25% by weight; a wetting agent in a range from 0.1 to 1.00% by weight; a zinc stearate in a range from 1.0 to 2.0% by weight; optionally, at least one pigment in a range from 1.0 to 8.0% by weight; a flame retardant in a range from 30.0 to 73.0% by weight; a thickener in a range from 0.1 to 1.0% by weight; a glass fiber in a range from 10.0 to 30.0% by weight; and a thermoplastic powder in a range of 0.1 to 2.5% by weight.
    • 一种用于制备外壳的片状模塑料,其包含基于20重量%至28.0重量%的基础树脂; 3.0〜7.0重量%的热塑性树脂; 苯乙烯单体的范围为0.01-2.5重量%; 0.1至0.7重量%的第一催化剂; 0.01至0.3重量%的第二催化剂; 0.01至0.25重量%的催化剂改性剂; 0.01至0.25重量%的抑制剂; 0.01至0.25重量%的UV吸收剂; 润湿剂的范围为0.1至1.00重量%; 硬脂酸锌为1.0-2.0重量%; 任选地,至少一种颜料的范围为1.0-8.0重量%; 阻燃剂的范围为30.0至73.0重量%; 浓度为0.1〜1.0重量%的增稠剂; 10.0〜30.0重量%的玻璃纤维; 和0.1〜2.5重量%的热塑性粉末。