Mathematical modeling of helicopter aerobatic maneuvers

被引：7

作者：

Cao, YH ^{[1
]}

Zhang, GL ^{[1
]}

Su, Y ^{[1
]}

机构：

[1] Beijing Univ Aeronaut & Astronaut, Dept Flight Vehicle Design & Appl Mech, Beijing 100083, Peoples R China

来源：

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY | 2004年 / 76卷 / 02期

关键词：

helicopters; flight; kinematics; dynamics; mathematical modelling;

D O I：

10.1108/00022660410526033

中图分类号：

V [航空、航天];

学科分类号：

08 [工学]; 0825 [航空宇航科学与技术];

摘要：

This paper describes the typical maneuvering courses of helicopters with mathematics systematically and presents the formulas and approaches for calculating the dynamics characteristics. A set of generalized equations which govern the kinematics and dynamics of helicopters in maneuvering flight is given. Three aerobatic maneuvers for loop, roll and turn are specially analyzed in detail and the sample calculations are presented. The method established in this paper is of practical significance for aerobatic employment and design of helicopters.

引用

页码：170 / 178

页数：9

共 17 条

[1]

Helicopter manoeuvre gaming simulation and mathematical inverse solution [J].