trick_euler; /* measured in units of TAU */
float trick_time;
+#if 0
m3x3f velocity_bias,
velocity_bias_pstep;
v3f apex;
+#endif
+
v3f up_dir;
v3f head_position;
int charging_jump, jump_dir;
float jump_charge;
- double jump_time;
+ double jump_time;
double start_push,
cur_push;
v3f prev_pos;
+
+ /* initial launch conditions */
+ double air_start;
+ v3f air_init_v,
+ air_init_co;
}
state,
state_gate_storage;
v3f log[50];
v3f n;
v3f apex;
+ v3f v;
+
int log_length;
float score,
land_dist;