摘要
Problems in modeling of sub-mini aerial vehicles(SMAV) are discussed in this paper. Contraposing properties of SMAV, various factors affecting dynamic performances and the airplane control are analyzed. Based on experiments, simulations, and computations, a corrected result for dynamic characteristics of fixed-wing SMAV and several instances of simulation are given, and the model of control and multi-stage PD control law are given too.
Problems in modeling of sub-mini aerial vehicles(SMAV) are discussed in this paper. Contraposing properties of SMAV, various factors affecting dynamic performances and the airplane control are analyzed. Based on experiments, simulations, and computations, a corrected result for dynamic characteristics of fixed-wing SMAV and several instances of simulation are given, and the model of control and multi-stage PD control law are given too.
基金
ProjectsupportedbytheNationalHigh TechnologyResearchandDevelopmentProgramofChina (GrantNo .2 0 0 1AA42 2 160 )andtheDevelopmentFoundationofShanghaiMunicipalCommis sionofEducation (GrantNo .0 2AK2 0 )