The problem of the integrated guidance and control (IGC) design for strap-down missile with the field-of-view (FOV) constraint is solved by using the integral barrier Lyapunov function (iBLF) and the sliding mode control theory. Firstly, the nonlinear and uncertainty state equation with non-strict feedback form for IGC design is derived by using the strap-down decoupling strategy. Secondly, a novel adaptive finite time disturbance observer is proposed to estimate the uncertainties based on an improved adaptive gain super twisting algorithm. Thirdly, the special time-varying sliding variable is designed and the iBLF is employed to handle the problem of FOV constraint. Theoretical derivation and simulation show that the IGC system is globally uniformly ultimately bounded and the FOV angle constraint is also guaranteed not only during the reaching phase but also during the sliding mode phase.
BhatSBernsteinD (1998) Continuous finite-time stabilization of the translational and rotational double integrators. IEEE Transactions on Automatic Control43(5): 678–682.
2.
BulentOAltugU (2012) Comparison of the strapdown and gimbaled seekers utilized in aerial applications. In: Infrared Technology and Applications XXXVIII, vol. 8353 of Proceedings of SPIE, Maryland, USA, May 2012. SPIE Publisher.
3.
ChenJLiQD, et al. (2016) Integrated guidance and control design based on a reference model. International Journal of Control Automation and Systems14(5): 1299–1308.
4.
ChenWH (2003) Disturbance observer based control for nonlinear systems. IEEE Transactions on Mechatronics9(4): 706–710.
5.
DavilaJFridmanLLevantA (2005) Second-order sliding-mode observer for mechanical systems. IEEE Transactions on Automatic Control50(11): 1785–1789
6.
FengYYuXH, et al.(2013) On nonsingular terminal sliding-mode control of nonlinear systems. Automatica49(6): 1715–1722.
7.
HallCEShtesselYB (2006) Sliding mode observer-based control for a reusable launch vehicle. Journal of Guidance, Control, and Dynamics29(6): 1315–1328.
8.
HeSMWangWWangJ (2016) Three-dimensional multivariable integrated guidance and control design for maneuvering targets interception. Journal of the Franklin Institute353(16): 4330–4350.
9.
HouMZLiangXLDuanGR (2013) Adaptive block dynamic surface control for integrated missile guidance and autopilot. Chinese Journal of Aeronautics26(3): 741–750.
10.
KimBCaliseASattigeriR (2007) Adaptive integrated guidance and control design for line-of-sight-based formation flight. Journal of Guidance, Control and Dynamics30(5): 1388–1398.
11.
KumerSRaoSGhoseD (2012) Sliding-mode guidance and control for all-aspect interceptors with terminal angle constraints. Journal of Guidance, Control and Dynamics35(4): 1230–1246.
12.
LeeSAnnS, et al. (2019) Capturability of guidance laws for interception of nonmaneuvering target with field-of-view limit. Journal of Guidance, Control, and Dynamics42(4): 869–884.
13.
LeeSChoNKimY (2020) Impact-time-control guidance strategy with a composite structure considering the seeker’s field-of-view constraint. Journal of Guidance, Control, and Dynamics, 43(8): 1566–1574.
14.
LeeCHyunC, et al. (2013) A hybrid guidance law for a strapdown seeker to maintain lock-on conditions against high speed targets. Journal of Electrical Engineering and Technology8(1): 190–196.
15.
LeeSKimY (2020) Capturability of impact-angle control composite guidance law considering field-of-view limit. IEEE Transactions on Aerospace and Electronic Systems56(2): 1077–1093.
16.
LiuJXGaoYB, et al. (2019) Disturbance-observer-based control for air management of PEM fuel cell systems via sliding mode technique. IEEE Transactions on Control Systems Technology27(3): 1129–1138.
17.
LiuJXLaghroucheSWackM (2013) Adaptive higher order sliding mode observer-based fault reconstruction for a class of nonlinear uncertain systems. In: Proceedings of 52nd IEEE Conference on Decision and Control, Florence, Italy, 10–13 December 2014, pp. 5668–5673. USA: IEEE.
18.
MohamedGSofifianeANicolasL (2018) Adaptive super twisting extended state observer based sliding mode control for diesel engine air path subject to matched and unmatched disturbance, Mathematics and Computers in Simulation151: 111–130.
19.
NageshIEdwardsC (2014) A multivariable super-twisting sliding mode approach, Automatica50(3): 984–988.
20.
ParkBKimTTahkM (2013) Optimal impact angle control guidance law considering the seeker’s field-of-view limits. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering227(8): 1347–1364.
21.
QiZK (2004) Guided Weapon Control System. 2nd Edn.Beijing: Institute of Technology Press.
22.
RatnooA (2016) Analysis of two-stage proportional navigation with heading constraints. Journal of Guidance Control and Dynamics39(1): 156–197.
23.
SangDTahkM (2009) Guidance law switching logic considering the seeker’s field-of-view limits. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering223(8): 1049–1058.
24.
SunGHWuLG, et al.(2018) Practical tracking control of linear motor via fractional-order sliding mode. Automatica94: 221–235.
25.
SunGHMaZQ(2017) Practical tracking control of linear motor with adaptive fractional order terminal sliding mode control. IEEE/ASME Transactions on Mechatronics, 22(6): 2643–2653.
26.
ShafermanV (2017) Optimal guidance with an in route look-angle constraint. In: AIAA Guidance, Navigation, and Control Conference, Grapevine, TX, United States, 9–13 January 2017. USA: AIAA.
27.
ShaoXLWangHL (2015) Back-stepping active disturbance rejection control design for integrated missile guidance and control system via reduced-order ESO. ISA Transactions57: 10–22.
28.
ShtesselYBFridmanLZinoberA (2008) Higher order sliding modes. International Journal of Robust and Nonlinear Control18(4–5): 381–384.
29.
SongHTZhangT (2016) Fast robust integrated guidance and control design of interceptors. IEEE Transactions on Control Systems Technology24(1): 349–356
30.
TeeKPGeSS (2012) Control of state-constrained nonlinear systems using integral barrier Lyapunov functionals. In: Proceedings of the 51st IEEE Conference on Decision and Control, Maui, HI, USA, 10–13 December 2012, pp. 3239–3244. USA: IEEE.
31.
TeeKPGeSSTayE (2008) Barrier Lyapunov functions for the control of output-constrained nonlinear systems. Automatica45(4): 918–927.
32.
VairavanARatnooA (2017) A non-switching guidance law for impact angle constrained interception of moving targets. In: AIAA Guidance, Navigation, and Control Conference, Grapevine, TX, United States, 9–13 January 2017. USA: AIAA.
33.
WangHDaleyS (1996) Actuator fault diagnosis: An adaptive observer-based technique. IEEE Transactions on Automatic Control41: 1073–1078.
34.
WangJHLiuLH, et al. (2016) Integrated guidance and control for hypersonic vehicles in dive phase with multiple constraints. Aerospace Science and Technology53: 103–115.
35.
WangXZhengYLinH (2015) Integrated guidance and control law for cooperative attack of multiple missiles. Aerospace Science and Technology42: 1–11.
36.
WangXLZhangYAWuHL (2016) Sliding mode control based impact angle control guidance considering the seeker’s field-of-view constraint. ISA Transactions61: 49–59.
37.
YangZWangHLinDF (2016) Time-varying biased proportional guidance with seeker’s field-of-view limit. International Journal of Aerospace Engineering: 9272019.
38.
YuSYuX, et al. (2005) Continuous finite time control for robotic manipulators with terminal sliding mode. Automatica41(11): 1957–1964.
39.
ZhangCWuYJ (2016) Nonsingular terminal dynamic surface control based integrated guidance and control design and simulation. ISA Transactions63: 112–120.
40.
ZhangYWangXWuH (2016) Impact time control guidance with field-of-view constraint accounting for uncertain system lag. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering230(3): 515–529.
41.
ZhaoBXuSY, et al. (2019) Integrated strap-down missile guidance and control based on neural network disturbance observer. Aerospace Science and Technology84: 170–181.
42.
ZhaoBZhouJ (2015) Attitude dynamics aiding for line-of-sight angular rate reconstruction of strap-down seeker. In: Proceedings of the 34th Chinese Control Conference, Hangzhou, China, 28–30 July 2015, pp. 5079–5083. IEEE.
43.
ZhaoBZhouJ (2016) Smooth adaptive finite time guidance law with impact angle constraints. International Journal of Aerospace Engineering2016: 5730168.
44.
ZhaoYWangJH, et al. (2019) Adaptive sliding mode fault-tolerant control for type-2 fuzzy systems with distributed delays. Information Sciences473: 227–238.
