代码搜索：Acceleration
找到约 615 项符合「Acceleration」的源代码
代码结果 615
www.eeworm.com/read/477110/6747961
h frne.h
/**
* \file frne.h
* \author Peter Corke
* \brief Definitions for MEX file
*
*/
/*
* Copyright (C) 1999-2008, by Peter I. Corke
*
* This file is part of The Robotics Toolbox for Matlab (RTB).
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m jtraj.m
%JTRAJ Compute a joint space trajectory between two points
%
% [Q QD QDD] = JTRAJ(Q0, Q1, N)
% [Q QD QDD] = JTRAJ(Q0, Q1, N, QD0, QD1)
% [Q QD QDD] = JTRAJ(Q0, Q1, T)
% [Q QD QDD] = JTRAJ(Q0, Q1, T, Q
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cpp demo13_2.cpp
// DEMO13_2.CPP - acceleration demo
// to compile make sure to include DDRAW.LIB, DSOUND.LIB,
// DINPUT.LIB, WINMM.LIB, and of course the T3DLIB files
// INCLUDES ////////////////////////////////
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cpp listing1.cpp
/* Copyright (C) Gari Biasillo, 2001.
* All rights reserved worldwide.
*
* This software is provided "as is" without express or implied
* warranties. You may freely copy and compile this sour
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m xppva.m
% xppva.m
% Scope: This MATLAB program determines acceleration from the input data of
% time, position and velocity, and plots all relevant trajectory
%
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cpp demo13_2.cpp
// DEMO13_2.CPP - acceleration demo
// to compile make sure to include DDRAW.LIB, DSOUND.LIB,
// DINPUT.LIB, WINMM.LIB, and of course the T3DLIB files
// INCLUDES ////////////////////////////////
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cpp demo13_2.cpp
// DEMO13_2.CPP - acceleration demo
// to compile make sure to include DDRAW.LIB, DSOUND.LIB,
// DINPUT.LIB, WINMM.LIB, and of course the T3DLIB files
// INCLUDES ////////////////////////////////
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cpp demo13_2.cpp
// DEMO13_2.CPP - acceleration demo
// to compile make sure to include DDRAW.LIB, DSOUND.LIB,
// DINPUT.LIB, WINMM.LIB, and of course the T3DLIB files
// INCLUDES ////////////////////////////////
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m partic1.m
%partic1.m - given the mass and initial time-dependent positions of 3 particles,
%this script calculates the velocities, accelerations and their center of mass
%values. Type "help symbolic" within
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hlp gravity.hlp
-----------------------------------------------------------------
GRAVITY is a masked Simulink subsystem, used to compute the
forces along the aircraft's body axes, which arise due to gra-
vity. Th