摘要
根据冗余度确定的原则,推导出了飞控/惯导综合系统MIRA最优冗余结构设计的基本条件—结构矩阵必须满秩;进而对结构矩阵的最优结构设计做了详细的推证。
On the base of the principle of determination redundancy, this paper derives the basic condition for the design of the optimal redundant structure for the Flight-control/Inertial integrated system MIRAstructure matrix should be all rank; further discusses the design of the optimal structure for structure matrix.
出处
《弹箭与制导学报》
CSCD
北大核心
2003年第1期21-23,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
基金
航空基金资助