Re: [Paparazzi-devel] control modes of fixed-wing aircrafts

[wertrrte]

Here is the possible values of the 'mode' variables.

lateral_mode:
#define LATERAL_MODE_MANUAL    0
#define LATERAL_MODE_ROLL_RATE 1
#define LATERAL_MODE_ROLL      2
#define LATERAL_MODE_COURSE    3
#define LATERAL_MODE_NB        4

pprz_mode:
#define  PPRZ_MODE_MANUAL 0
#define  PPRZ_MODE_AUTO1 1
#define  PPRZ_MODE_AUTO2 2
#define  PPRZ_MODE_HOME 3
#define  PPRZ_MODE_GPS_OUT_OF_ORDER 4
#define  PPRZ_MODE_NB 5

horizontal_mode:
#define HORIZONTAL_MODE_WAYPOINT 0
#define HORIZONTAL_MODE_ROUTE 1
#define HORIZONTAL_MODE_CIRCLE 2

nav_mode:
#define NAV_MODE_ROLL 1
#define NAV_MODE_COURSE 2

v_ctl_mode:
#define V_CTL_MODE_MANUAL        0
#define V_CTL_MODE_AUTO_THROTTLE 1
#define V_CTL_MODE_AUTO_CLIMB    2
#define V_CTL_MODE_AUTO_ALT      3
#define V_CTL_MODE_NB            4

I want to know, for example,if in different lateral_mode(2 and 3,e.g.),the
difference of the control behavior.This of course involves much details,so
any general idea or concept will be appreciated. 



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