#include "BodyEnvironment.hpp"
#include "Ground.hpp"
#include "RigidBody.hpp"
-
#include "Launchbar.hpp"
-#include <iostream>
-using namespace std;
namespace yasim {
+ static const float YASIM_PI2 = 3.14159265358979323846f/2;
+ static const float YASIM_PI = 3.14159265358979323846f;
+ static const float RAD2DEG = 180/YASIM_PI;
+
Launchbar::Launchbar()
{
int i;
for(i=0; i<3; i++)
- _launchbar_mount[i] = _holdback_mount[i] = _force[i] = 0;
+ _launchbar_mount[i] = _holdback_mount[i] = _launchbar_force[i]
+ = _holdback_force[i] = 0;
for(i=0; i<2; i++)
_global_ground[i] = 0;
_global_ground[2] = 1;
_holdback_length = 2.0;
_down_ang = 0.0;
_up_ang = 0.0;
+ _ang = 0.0;
_extension = 0.0;
- _frac = 0.0;
+ _frac = _h_frac =0.0;
_launch_cmd = false;
_pos_on_cat = 0.0;
_state = Unmounted;
+ _strop = false;
+ _acceleration = 0.25;
}
void Launchbar::setLaunchbarMount(float* position)
_length = length;
}
+ void Launchbar::setHoldbackLength(float length)
+ {
+ _holdback_length = length;
+ }
+
void Launchbar::setDownAngle(float ang)
{
_down_ang = ang;
_launch_cmd = cmd;
}
+void Launchbar::setAcceleration(float acceleration)
+{
+ _acceleration = acceleration;
+}
+
void Launchbar::setGlobalGround(double *global_ground)
{
int i;
for(i=0; i<3; i++) out[i] = _launchbar_mount[i];
}
+ float Launchbar::getLaunchbarPos(int i)
+ {
+ return _launchbar_mount[i];
+ }
+
void Launchbar::getHoldbackMount(float* out)
{
int i;
for(i=0; i<3; i++) out[i] = _holdback_mount[i];
}
+ float Launchbar::getHoldbackPos(int j)
+ {
+ return _holdback_mount[j];
+ }
+
+ float Launchbar::getHoldbackLength(void)
+ {
+ return _holdback_length;
+ }
+
float Launchbar::getLength(void)
{
return _length;
return _up_ang;
}
+ float Launchbar::getAngle(void)
+ {
+ return _ang;
+ }
+
+ float Launchbar::getHoldbackAngle(void)
+ {
+ return _h_ang;
+ }
float Launchbar::getExtension(void)
{
return _extension;
}
-void Launchbar::getForce(float* force, float* off)
+ void Launchbar::getForce(float* force1, float* off1,
+ float* force2, float* off2)
+ {
+ Math::set3(_launchbar_force, force1);
+ Math::set3(_launchbar_mount, off1);
+ Math::set3(_holdback_force, force2);
+ Math::set3(_holdback_mount, off2);
+ }
+
+ const char* Launchbar::getState(void)
+ {
+ switch (_state) {
+ case Arrested:
+ return "Engaged";
+ case Launch:
+ return "Launching";
+ case Completed:
+ return "Completed";
+ default:
+ return "Disengaged";
+ }
+ }
+
+ bool Launchbar::getStrop(void)
{
- Math::set3(_force, force);
- Math::set3(_launchbar_mount, off);
+ return _strop;
}
float Launchbar::getCompressFraction()
return _frac;
}
+ float Launchbar::getHoldbackCompressFraction()
+ {
+ return _h_frac;
+ }
+
void Launchbar::getTipPosition(float* out)
{
// The launchbar tip in local coordinates.
- float ang = _frac*(_down_ang - _up_ang) + _up_ang;
- float pos_tip[3] = { _length*Math::cos(ang), 0.0,-_length*Math::sin(ang) };
- Math::add3(_launchbar_mount, pos_tip, out);
+
+ _ang = _frac*(_down_ang - _up_ang ) + _up_ang ;
+ float ptip[3] = { _length*Math::cos(_ang), 0, -_length*Math::sin(_ang) };
+ Math::add3(_launchbar_mount, ptip, out);
+ }
+
+ float Launchbar::getTipPos(int i)
+ {
+ float pos_tip[3];
+ getTipPosition(pos_tip);
+ return pos_tip[i];
+ }
+
+ void Launchbar::getHoldbackTipPosition(float* out)
+ {
+ // The holdback tip in local coordinates.
+ _h_ang = _h_frac*(_down_ang - _up_ang) + _up_ang;
+ float htip[3] = { -_length*Math::cos(_h_ang), 0, -_length*Math::sin(_h_ang) };
+ Math::add3(_holdback_mount, htip, out);
+ }
+
+ float Launchbar::getHoldbackTipPos(int i)
+ {
+ float pos_tip[3];
+ getHoldbackTipPosition(pos_tip);
+ return pos_tip[i];
}
+
void Launchbar::getTipGlobalPosition(State* s, double* out)
{
// The launchbar tip in local coordinates.
float tmp[3];
Math::mul3(perc, lendvels[0], lvel);
- Math::mul3(1.0-perc, lendvels[1], tmp);
+ Math::mul3(1.0f-perc, lendvels[1], tmp);
Math::add3(tmp, lvel, lvel);
}
{
// Init the return values
int i;
- for(i=0; i<3; i++) _force[i] = 0;
+ for(i=0; i<3; i++) _launchbar_force[i] = 0;
+ for(i=0; i<3; i++) _holdback_force[i] = 0;
if (_state != Unmounted)
_extension = 1;
if(_extension <= 0)
return;
- if (_extension < _frac)
- _frac = _extension;
+ // For the first guess, the position fraction is equal to the
+ // extension value.
+ _frac = _h_frac = _extension;
- // The launchbar tip in global coordinates.
- double launchbar_pos[3];
- getTipGlobalPosition(s, launchbar_pos);
+ // The ground plane transformed to the local frame.
+ float ground[4];
+ s->planeGlobalToLocal(_global_ground, ground);
+
+ // The launchbar tip in local coordinates.
+ float ltip[3];
+ getTipPosition(ltip);
- // If the launchbars tip is less extended than it could be.
- if(_frac < _extension) {
// Correct the extension value for no intersection.
- // Compute the distance of the mount point from the ground plane.
- double a = - _global_ground[3] + launchbar_pos[0]*_global_ground[0]
- + launchbar_pos[1]*_global_ground[1]
- + launchbar_pos[2]*_global_ground[2];
- if(a < _length) {
- float ang = Math::asin(a/_length);
+
+ // Check if the tip will intersect the ground or not. That is, compute
+ // the distance of the tip to the ground plane.
+ float tipdist = ground[3] - Math::dot3(ltip, ground);
+ if(0 <= tipdist) {
+ _frac = _extension;
+ } else {
+ // Compute the distance of the launchbar mount point from the
+ // ground plane.
+ float mountdist = ground[3] - Math::dot3(_launchbar_mount, ground);
+
+ // Compute the distance of the launchbar mount point from the
+ // ground plane in the x-z plane. It holds:
+ // mountdist = mountdist_xz*cos(angle(normal_yz, e_z))
+ // thus
+ float mountdist_xz = _length;
+ if (ground[2] != 0) {
+ float nrm_yz = Math::sqrt(ground[1]*ground[1]+ground[2]*ground[2]);
+ mountdist_xz = -mountdist*nrm_yz/ground[2];
+ }
+
+ if (mountdist_xz < _length) {
+ // the launchbar points forward, so we need to change the signs here
+ float ang = -Math::asin(mountdist_xz/_length)
+ + Math::atan2(ground[2], ground[0]) + YASIM_PI2;
+ ang = -ang;
_frac = (ang - _up_ang)/(_down_ang - _up_ang);
- } else
- // FIXME: this will jump
+ } else {
_frac = _extension;
}
+ }
+
+ // Now do it again for the holdback
+
+ // The holdback tip in local coordinates.
+ float htip[3];
+ getHoldbackTipPosition(htip);
+
+ // Check if the tip will intersect the ground or not. That is, compute
+ // the distance of the tip to the ground plane.
+ float h_tipdist = ground[3] - Math::dot3(htip, ground);
+ if (0 <= h_tipdist) {
+ _h_frac = _extension;
+ } else {
+ // Compute the distance of the holdback mount point from the ground
+ // plane.
+ float h_mountdist = ground[3] - Math::dot3(_holdback_mount, ground);
+
+ // Compute the distance of the holdback mount point from the ground
+ // plane in the x-z plane. It holds:
+ // mountdist = mountdist_xz*cos(angle(normal_yz, e_z))
+ // thus
+ float h_mountdist_xz = _holdback_length;
+ if (ground[2] != 0) {
+ float nrm_yz = Math::sqrt(ground[1]*ground[1]+ground[2]*ground[2]);
+ h_mountdist_xz = -h_mountdist*nrm_yz/ground[2];
+ }
+
+ if (h_mountdist_xz < _holdback_length) {
+ float h_ang = Math::asin(h_mountdist_xz/_holdback_length)
+ + Math::atan2(ground[2], ground[0]) + YASIM_PI2;
+ _h_frac = (h_ang - _up_ang)/(_down_ang - _up_ang);
+ } else {
+ _h_frac = _extension;
+ }
+ }
- // Recompute the launchbar tip.
float llb_mount[3];
getTipPosition(llb_mount);
+
// The launchbar tip in global coordinates.
+ double launchbar_pos[3];
s->posLocalToGlobal(llb_mount, launchbar_pos);
double end[2][3]; float vel[2][3];
return;
// Compute the positions of the catapult start and endpoints in the
- // local coordiante system
+ // local coordinate system
float lend[2][3];
s->posGlobalToLocal(end[0], lend[0]);
s->posGlobalToLocal(end[1], lend[1]);
float llbdir[3];
Math::sub3(llbtip, _launchbar_mount, llbdir);
float lblen = Math::mag3(llbdir);
- Math::mul3(1.0/lblen, llbdir, llbdir);
+ Math::mul3(1.0f/lblen, llbdir, llbdir);
// Check if we are near enough to the cat.
- if (_state == Unmounted && dist < 0.5) {
- // croase approximation for the velocity of the launchbar.
+ if (_state == Unmounted && dist < 0.6) {
+ // coarse approximation for the velocity of the launchbar.
// Might be sufficient because arresting at the cat makes only
// sense when the aircraft does not rotate much.
float lv_mount[3];
double dd[2][3]; float fd[2][3]; double ghldbkpos[3];
s->posLocalToGlobal(_holdback_mount, ghldbkpos);
float hbdist = g_cb->getCatapult(ghldbkpos, dd, fd);
- float offset = -Math::sqrt(_holdback_length*_holdback_length - hbdist*hbdist);
- _pos_on_cat = getPercentPosOnCat(_holdback_mount, offset, lend);
+ // don't let the calculation go -ve here
+ if (_holdback_length*_holdback_length - hbdist*hbdist < 0)
+ return;
+ float offset = -Math::sqrt(_holdback_length*_holdback_length
+ - hbdist*hbdist);
+ _pos_on_cat = getPercentPosOnCat(_holdback_mount, offset, lend);
// We cannot arrest if we are not at the start of the cat.
- if (_pos_on_cat < 0.0 || 0.2 < _pos_on_cat)
+ if (_pos_on_cat < 0.0 || 0.4 < _pos_on_cat)
return;
// Now we are arrested at the cat.
if (_state == Arrested) {
// Now apply a constant tension from the catapult over the launchbar.
- Math::mul3(2.0, llbdir, _force);
+ Math::mul3(2.0, llbdir, _launchbar_force);
// If the distance from the holdback mount at the aircraft to the
// holdback mount on the cat is larger than the holdback length itself,
// the holdback applies a force to the gear.
if (_holdback_length < hldbklen) {
- // croase approximation for the velocity of the holdback mount
+ // coarse approximation for the velocity of the holdback mount
// at the gear.
// Might be sufficient because arresting at the cat makes only
// sense when the aircraft does not rotate much.
// The spring force the holdback will apply to the gear
float tmp[3];
- Math::mul3(1e1*(hldbklen - _holdback_length), lhldbkdir, tmp);
- Math::add3(tmp, _force, _force);
+ Math::mul3(10.f*(hldbklen - _holdback_length), lhldbkdir,
+ _holdback_force);
// The damping force here ...
Math::mul3(2e0, lvhldbk, tmp);
- Math::sub3(_force, tmp, _force);
+ Math::sub3(_holdback_force, tmp, _holdback_force);
}
- if (_launch_cmd)
+ if (_launch_cmd) {
_state = Launch;
+ _strop = false;
+ }
}
if (_state == Launch) {
// Now apply a constant tension from the catapult over the launchbar.
- Math::mul3(25.0, llbdir, _force);
+ // We modify the max accleration 100 m/s^2 by the normalised input
+ //SG_LOG(SG_FLIGHT, SG_ALERT, "acceleration " << 100 * _acceleration );
+ Math::mul3(100 * _acceleration, llbdir, _launchbar_force);
+
+ if (1.0 < dist) {
+ _state = Completed;
+ }
+ }
+
+ if (_state == Completed) {
+ // Wait until the strop has cleared the deck
+ // This is a temporary fix until we come up with something better
- if (1.0 < dist)
+ if (_frac > 0.8) {
_state = Unmounted;
+ _strop = true;
+ }
}
// Scale by the mass. That keeps the stiffness in reasonable bounds.
float mass = body->getTotalMass();
- Math::mul3(mass, _force, _force);
+ Math::mul3(mass, _launchbar_force, _launchbar_force);
+ Math::mul3(mass, _holdback_force, _holdback_force);
}
}; // namespace yasim
projects / flightgear.git / blobdiff