TY - GEN
T1 - IAC-15,A3,IP,18,x28460 Onboard waypoint planning based mars predictive entry guidance with path constraints
AU - Long, Jiateng
AU - Gao, Ai
AU - Cui, Pingyuan
N1 - Publisher Copyright:
© Copyright 2015 by International Astronautical Federation. All rights reserved.
PY - 2015
Y1 - 2015
N2 - The predictive entry guidance method emerges and has been focused on in recent years for the potential of dealing with unexpected circumstances onboard automatically and improving delivery accuracy during Mars atmospheric entry phase. For the design of predictive entry guidance, one of the difficulties to be faced with is to satisfy the path constraints including load factor, heat flux, etc. In view of path constraints satisfaction through Martian atmosphere, a method of planning waypoint onboard is introduced to enhance the capability of predictive entry guidance to meet both of the path constrains and the terminal accuracy at the same time. As far as the knowledge of authors, in predictive entry guidance, the methods presented up to now on solving path constraints arc based on the idea of tracking the ceiling of the constraint passively when it is to be reached, and it may result in the saturation of guidance command. However, the idea of onboard waypoint planning is to deal with the path constraints actively and prospectively by taking full use of the predictive capability of guidance algorithm. First of all, the sufficient condition of satisfying path constraints is presented in the altitude-velocity space analytically, with the exponential density model of Martian atmosphere. On the basis of this sufficient condition, when path constraints are predicted to be violated, the waypoint planning algorithm is adopted to generate a waypoint and then the vehicle will be guided to fly to it firstly to guarantee the path constraints. With one or several times of waypoint planning, the vehicle will pass through die period during which path constraints may be violated and finally to the predetermined position of parachute deployment. With the picccwisc predictive guidance process, both of the path constraints and the terminal constraints will finally be met. Moreover, the onboard calculation load of numerical integration will be relieved by inserting the waypoint with the cost of the waypoint generation only.
AB - The predictive entry guidance method emerges and has been focused on in recent years for the potential of dealing with unexpected circumstances onboard automatically and improving delivery accuracy during Mars atmospheric entry phase. For the design of predictive entry guidance, one of the difficulties to be faced with is to satisfy the path constraints including load factor, heat flux, etc. In view of path constraints satisfaction through Martian atmosphere, a method of planning waypoint onboard is introduced to enhance the capability of predictive entry guidance to meet both of the path constrains and the terminal accuracy at the same time. As far as the knowledge of authors, in predictive entry guidance, the methods presented up to now on solving path constraints arc based on the idea of tracking the ceiling of the constraint passively when it is to be reached, and it may result in the saturation of guidance command. However, the idea of onboard waypoint planning is to deal with the path constraints actively and prospectively by taking full use of the predictive capability of guidance algorithm. First of all, the sufficient condition of satisfying path constraints is presented in the altitude-velocity space analytically, with the exponential density model of Martian atmosphere. On the basis of this sufficient condition, when path constraints are predicted to be violated, the waypoint planning algorithm is adopted to generate a waypoint and then the vehicle will be guided to fly to it firstly to guarantee the path constraints. With one or several times of waypoint planning, the vehicle will pass through die period during which path constraints may be violated and finally to the predetermined position of parachute deployment. With the picccwisc predictive guidance process, both of the path constraints and the terminal constraints will finally be met. Moreover, the onboard calculation load of numerical integration will be relieved by inserting the waypoint with the cost of the waypoint generation only.
UR - http://www.scopus.com/inward/record.url?scp=84991377559&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:84991377559
T3 - Proceedings of the International Astronautical Congress, IAC
SP - 1423
EP - 1430
BT - 66th International Astronautical Congress 2015, IAC 2015
PB - International Astronautical Federation, IAF
T2 - 66th International Astronautical Congress 2015: Space - The Gateway for Mankind's Future, IAC 2015
Y2 - 12 October 2015 through 16 October 2015
ER -