船舶力学
船舶力學
선박역학
JOURNAL OF SHIP MECHANICS
2013年
1期
19-28
,共10页
王芳%潘再生%万磊%徐玉如
王芳%潘再生%萬磊%徐玉如
왕방%반재생%만뢰%서옥여
动力定位%深海钻井平台%推力分配%最优化%全方位推进器%非线性约束
動力定位%深海鑽井平檯%推力分配%最優化%全方位推進器%非線性約束
동력정위%심해찬정평태%추력분배%최우화%전방위추진기%비선성약속
dynamic positioning%deepwater drilling rig%thrust allocation%optimization%azimuth thruster%nonlinear constraint
深海动力定位主要依靠海洋结构物的自身动力来抵抗外界环境力的干扰,推进器系统作为动力定位系统的执行机构,其工作性能的好坏将直接影响到最终的定位效果.文章简述了推力分配在动力定位实时控制系统中的功能,并归纳了用非线性规划求解最优化问题可能存在的困难.针对981钻井平台冗余的全方位推力器配置,引入扩展推力将推力分配的非线性等式约束转化为线性等式约束,提出了基于扩展推力的拉格朗日最小平方优化的显性解,在最优扩展推力的基础上对每个推进器的最大推力、推力变化以及全方位推进器方向角的最大转动变化率均作了限制.仿真结果表明该推力分配策略切实可行,对实时控制系统的内存无特别要求,定位性能较好.
深海動力定位主要依靠海洋結構物的自身動力來牴抗外界環境力的榦擾,推進器繫統作為動力定位繫統的執行機構,其工作性能的好壞將直接影響到最終的定位效果.文章簡述瞭推力分配在動力定位實時控製繫統中的功能,併歸納瞭用非線性規劃求解最優化問題可能存在的睏難.針對981鑽井平檯冗餘的全方位推力器配置,引入擴展推力將推力分配的非線性等式約束轉化為線性等式約束,提齣瞭基于擴展推力的拉格朗日最小平方優化的顯性解,在最優擴展推力的基礎上對每箇推進器的最大推力、推力變化以及全方位推進器方嚮角的最大轉動變化率均作瞭限製.倣真結果錶明該推力分配策略切實可行,對實時控製繫統的內存無特彆要求,定位性能較好.
심해동력정위주요의고해양결구물적자신동력래저항외계배경력적간우,추진기계통작위동력정위계통적집행궤구,기공작성능적호배장직접영향도최종적정위효과.문장간술료추력분배재동력정위실시공제계통중적공능,병귀납료용비선성규화구해최우화문제가능존재적곤난.침대981찬정평태용여적전방위추력기배치,인입확전추력장추력분배적비선성등식약속전화위선성등식약속,제출료기우확전추력적랍격랑일최소평방우화적현성해,재최우확전추력적기출상대매개추진기적최대추력、추력변화이급전방위추진기방향각적최대전동변화솔균작료한제.방진결과표명해추력분배책략절실가행,대실시공제계통적내존무특별요구,정위성능교호.
@@@@Dynamically Positioned vessels counteract environmental loads to maintain its position exclu-sively by means of its own active actuators in deepwater. The thruster system is regarded as a critical sys-tem with respect to positioning performance and safety. The role of control/force allocation in the real-time control hierarchy of DP system is addressed, and the difficulties of iterative solution for overactuated control allocation by using nonlinear programming optimization are pointed out. An explicit solution to the least square optimization with respect to extended thruster was presented to minimize power consumption for a deepwater drilling rig with redundant azimuth thrusters, the usage of extended thrust is to transform the nonlinear equal constraints to linear constrains. Since there are sector limitations for operation of the az-imuth thrusters, both amplitude and rate saturation, rate constrains on the azimuth angles and tear and ware are also taken into account. Simulation results show that the proposed thrust allocation scheme is applicable and reliable without specified requirements on storage space of memory and the control performance is satisfied with the proposed thrust allocation scheme.